Experimental and finite element studies on free vibration of cylindrical skew panels

Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental v...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Srinivasa, Chikkol V [verfasserIn] Suresh, Yalaburgi J [verfasserIn] Prema kumar, Wooday P [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2014

Schlagwörter:	Cylindrical skew panel Panel angle Skew angle Fiber orientation angle Antisymmetric laminate Finite element analysis Natural frequency

Übergeordnetes Werk:	Enthalten in: International journal of advanced structural engineering - Berlin : Springer, 2009, 6(2014), 1 vom: 21. Jan.
Übergeordnetes Werk:	volume:6 ; year:2014 ; number:1 ; day:21 ; month:01

Links:	Volltext

DOI / URN:	10.1186/2008-6695-6-1

Katalog-ID:	SPR032822421

Internformat


LEADER	01000caa a22002652 4500
001	SPR032822421
003	DE-627
005	20220111205428.0
007	cr uuu---uuuuu
008	201007s2014 xx \|\|\|\|\|o 00\| \|\|eng c
024	7		\|a 10.1186/2008-6695-6-1 \|2 doi
035			\|a (DE-627)SPR032822421
035			\|a (SPR)2008-6695-6-1-e
040			\|a DE-627 \|b ger \|c DE-627 \|e rakwb
041			\|a eng
082	0	4	\|a 620 \|a 690 \|q ASE
084			\|a 56.00 \|2 bkl
100	1		\|a Srinivasa, Chikkol V \|e verfasserin \|4 aut
245	1	0	\|a Experimental and finite element studies on free vibration of cylindrical skew panels
264		1	\|c 2014
336			\|a Text \|b txt \|2 rdacontent
337			\|a Computermedien \|b c \|2 rdamedia
338			\|a Online-Ressource \|b cr \|2 rdacarrier
520			\|a Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels.
650		4	\|a Cylindrical skew panel \|7 (dpeaa)DE-He213
650		4	\|a Panel angle \|7 (dpeaa)DE-He213
650		4	\|a Skew angle \|7 (dpeaa)DE-He213
650		4	\|a Fiber orientation angle \|7 (dpeaa)DE-He213
650		4	\|a Antisymmetric laminate \|7 (dpeaa)DE-He213
650		4	\|a Finite element analysis \|7 (dpeaa)DE-He213
650		4	\|a Natural frequency \|7 (dpeaa)DE-He213
700	1		\|a Suresh, Yalaburgi J \|e verfasserin \|4 aut
700	1		\|a Prema kumar, Wooday P \|e verfasserin \|4 aut
773	0	8	\|i Enthalten in \|t International journal of advanced structural engineering \|d Berlin : Springer, 2009 \|g 6(2014), 1 vom: 21. Jan. \|w (DE-627)684551314 \|w (DE-600)2649231-3 \|x 2008-6695 \|7 nnns
773	1	8	\|g volume:6 \|g year:2014 \|g number:1 \|g day:21 \|g month:01
856	4	0	\|u https://dx.doi.org/10.1186/2008-6695-6-1 \|z kostenfrei \|3 Volltext
912			\|a GBV_USEFLAG_A
912			\|a SYSFLAG_A
912			\|a GBV_SPRINGER
912			\|a GBV_ILN_20
912			\|a GBV_ILN_22
912			\|a GBV_ILN_23
912			\|a GBV_ILN_24
912			\|a GBV_ILN_31
912			\|a GBV_ILN_39
912			\|a GBV_ILN_40
912			\|a GBV_ILN_60
912			\|a GBV_ILN_62
912			\|a GBV_ILN_63
912			\|a GBV_ILN_65
912			\|a GBV_ILN_69
912			\|a GBV_ILN_70
912			\|a GBV_ILN_73
912			\|a GBV_ILN_95
912			\|a GBV_ILN_105
912			\|a GBV_ILN_110
912			\|a GBV_ILN_151
912			\|a GBV_ILN_161
912			\|a GBV_ILN_170
912			\|a GBV_ILN_213
912			\|a GBV_ILN_230
912			\|a GBV_ILN_285
912			\|a GBV_ILN_293
912			\|a GBV_ILN_370
912			\|a GBV_ILN_602
912			\|a GBV_ILN_2014
912			\|a GBV_ILN_2027
912			\|a GBV_ILN_4012
912			\|a GBV_ILN_4037
912			\|a GBV_ILN_4112
912			\|a GBV_ILN_4125
912			\|a GBV_ILN_4126
912			\|a GBV_ILN_4249
912			\|a GBV_ILN_4305
912			\|a GBV_ILN_4306
912			\|a GBV_ILN_4307
912			\|a GBV_ILN_4313
912			\|a GBV_ILN_4322
912			\|a GBV_ILN_4323
912			\|a GBV_ILN_4324
912			\|a GBV_ILN_4325
912			\|a GBV_ILN_4335
912			\|a GBV_ILN_4338
912			\|a GBV_ILN_4367
912			\|a GBV_ILN_4392
912			\|a GBV_ILN_4700
936	b	k	\|a 56.00 \|q ASE
951			\|a AR
952			\|d 6 \|j 2014 \|e 1 \|b 21 \|c 01

Indexfelder

author_variant	c v s cv cvs y j s yj yjs k w p p kwp kwpp
matchkey_str	article:20086695:2014----::xeietlnfnteeettdeofevbainfy
hierarchy_sort_str	2014
bklnumber	56.00
publishDate	2014
allfields	10.1186/2008-6695-6-1 doi (DE-627)SPR032822421 (SPR)2008-6695-6-1-e DE-627 ger DE-627 rakwb eng 620 690 ASE 56.00 bkl Srinivasa, Chikkol V verfasserin aut Experimental and finite element studies on free vibration of cylindrical skew panels 2014 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels. Cylindrical skew panel (dpeaa)DE-He213 Panel angle (dpeaa)DE-He213 Skew angle (dpeaa)DE-He213 Fiber orientation angle (dpeaa)DE-He213 Antisymmetric laminate (dpeaa)DE-He213 Finite element analysis (dpeaa)DE-He213 Natural frequency (dpeaa)DE-He213 Suresh, Yalaburgi J verfasserin aut Prema kumar, Wooday P verfasserin aut Enthalten in International journal of advanced structural engineering Berlin : Springer, 2009 6(2014), 1 vom: 21. Jan. (DE-627)684551314 (DE-600)2649231-3 2008-6695 nnns volume:6 year:2014 number:1 day:21 month:01 https://dx.doi.org/10.1186/2008-6695-6-1 kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2027 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4392 GBV_ILN_4700 56.00 ASE AR 6 2014 1 21 01
spelling	10.1186/2008-6695-6-1 doi (DE-627)SPR032822421 (SPR)2008-6695-6-1-e DE-627 ger DE-627 rakwb eng 620 690 ASE 56.00 bkl Srinivasa, Chikkol V verfasserin aut Experimental and finite element studies on free vibration of cylindrical skew panels 2014 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels. Cylindrical skew panel (dpeaa)DE-He213 Panel angle (dpeaa)DE-He213 Skew angle (dpeaa)DE-He213 Fiber orientation angle (dpeaa)DE-He213 Antisymmetric laminate (dpeaa)DE-He213 Finite element analysis (dpeaa)DE-He213 Natural frequency (dpeaa)DE-He213 Suresh, Yalaburgi J verfasserin aut Prema kumar, Wooday P verfasserin aut Enthalten in International journal of advanced structural engineering Berlin : Springer, 2009 6(2014), 1 vom: 21. Jan. (DE-627)684551314 (DE-600)2649231-3 2008-6695 nnns volume:6 year:2014 number:1 day:21 month:01 https://dx.doi.org/10.1186/2008-6695-6-1 kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2027 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4392 GBV_ILN_4700 56.00 ASE AR 6 2014 1 21 01
allfields_unstemmed	10.1186/2008-6695-6-1 doi (DE-627)SPR032822421 (SPR)2008-6695-6-1-e DE-627 ger DE-627 rakwb eng 620 690 ASE 56.00 bkl Srinivasa, Chikkol V verfasserin aut Experimental and finite element studies on free vibration of cylindrical skew panels 2014 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels. Cylindrical skew panel (dpeaa)DE-He213 Panel angle (dpeaa)DE-He213 Skew angle (dpeaa)DE-He213 Fiber orientation angle (dpeaa)DE-He213 Antisymmetric laminate (dpeaa)DE-He213 Finite element analysis (dpeaa)DE-He213 Natural frequency (dpeaa)DE-He213 Suresh, Yalaburgi J verfasserin aut Prema kumar, Wooday P verfasserin aut Enthalten in International journal of advanced structural engineering Berlin : Springer, 2009 6(2014), 1 vom: 21. Jan. (DE-627)684551314 (DE-600)2649231-3 2008-6695 nnns volume:6 year:2014 number:1 day:21 month:01 https://dx.doi.org/10.1186/2008-6695-6-1 kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2027 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4392 GBV_ILN_4700 56.00 ASE AR 6 2014 1 21 01
allfieldsGer	10.1186/2008-6695-6-1 doi (DE-627)SPR032822421 (SPR)2008-6695-6-1-e DE-627 ger DE-627 rakwb eng 620 690 ASE 56.00 bkl Srinivasa, Chikkol V verfasserin aut Experimental and finite element studies on free vibration of cylindrical skew panels 2014 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels. Cylindrical skew panel (dpeaa)DE-He213 Panel angle (dpeaa)DE-He213 Skew angle (dpeaa)DE-He213 Fiber orientation angle (dpeaa)DE-He213 Antisymmetric laminate (dpeaa)DE-He213 Finite element analysis (dpeaa)DE-He213 Natural frequency (dpeaa)DE-He213 Suresh, Yalaburgi J verfasserin aut Prema kumar, Wooday P verfasserin aut Enthalten in International journal of advanced structural engineering Berlin : Springer, 2009 6(2014), 1 vom: 21. Jan. (DE-627)684551314 (DE-600)2649231-3 2008-6695 nnns volume:6 year:2014 number:1 day:21 month:01 https://dx.doi.org/10.1186/2008-6695-6-1 kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2027 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4392 GBV_ILN_4700 56.00 ASE AR 6 2014 1 21 01
allfieldsSound	10.1186/2008-6695-6-1 doi (DE-627)SPR032822421 (SPR)2008-6695-6-1-e DE-627 ger DE-627 rakwb eng 620 690 ASE 56.00 bkl Srinivasa, Chikkol V verfasserin aut Experimental and finite element studies on free vibration of cylindrical skew panels 2014 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels. Cylindrical skew panel (dpeaa)DE-He213 Panel angle (dpeaa)DE-He213 Skew angle (dpeaa)DE-He213 Fiber orientation angle (dpeaa)DE-He213 Antisymmetric laminate (dpeaa)DE-He213 Finite element analysis (dpeaa)DE-He213 Natural frequency (dpeaa)DE-He213 Suresh, Yalaburgi J verfasserin aut Prema kumar, Wooday P verfasserin aut Enthalten in International journal of advanced structural engineering Berlin : Springer, 2009 6(2014), 1 vom: 21. Jan. (DE-627)684551314 (DE-600)2649231-3 2008-6695 nnns volume:6 year:2014 number:1 day:21 month:01 https://dx.doi.org/10.1186/2008-6695-6-1 kostenfrei Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2027 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4392 GBV_ILN_4700 56.00 ASE AR 6 2014 1 21 01
language	English
source	Enthalten in International journal of advanced structural engineering 6(2014), 1 vom: 21. Jan. volume:6 year:2014 number:1 day:21 month:01
sourceStr	Enthalten in International journal of advanced structural engineering 6(2014), 1 vom: 21. Jan. volume:6 year:2014 number:1 day:21 month:01
format_phy_str_mv	Article
institution	findex.gbv.de
topic_facet	Cylindrical skew panel Panel angle Skew angle Fiber orientation angle Antisymmetric laminate Finite element analysis Natural frequency
dewey-raw	620
isfreeaccess_bool	true
container_title	International journal of advanced structural engineering
authorswithroles_txt_mv	Srinivasa, Chikkol V @@aut@@ Suresh, Yalaburgi J @@aut@@ Prema kumar, Wooday P @@aut@@
publishDateDaySort_date	2014-01-21T00:00:00Z
hierarchy_top_id	684551314
dewey-sort	3620
id	SPR032822421
language_de	englisch
fullrecord	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR032822421</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20220111205428.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">201007s2014 xx \|\|\|\|\|o 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1186/2008-6695-6-1</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR032822421</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)2008-6695-6-1-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">620</subfield><subfield code="a">690</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">56.00</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Srinivasa, Chikkol V</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Experimental and finite element studies on free vibration of cylindrical skew panels</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2014</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Cylindrical skew panel</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Panel angle</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Skew angle</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Fiber orientation angle</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Antisymmetric laminate</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Finite element analysis</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Natural frequency</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Suresh, Yalaburgi J</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Prema kumar, Wooday P</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">International journal of advanced structural engineering</subfield><subfield code="d">Berlin : Springer, 2009</subfield><subfield code="g">6(2014), 1 vom: 21. Jan.</subfield><subfield code="w">(DE-627)684551314</subfield><subfield code="w">(DE-600)2649231-3</subfield><subfield code="x">2008-6695</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:6</subfield><subfield code="g">year:2014</subfield><subfield code="g">number:1</subfield><subfield code="g">day:21</subfield><subfield code="g">month:01</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://dx.doi.org/10.1186/2008-6695-6-1</subfield><subfield code="z">kostenfrei</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_SPRINGER</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_22</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_24</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_31</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_39</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_60</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_63</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_69</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_73</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_95</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_105</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_110</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_151</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_161</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_170</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_213</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_230</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_285</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_293</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_370</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_602</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2014</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2027</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4012</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4037</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4112</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4125</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4126</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4249</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4305</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4306</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4307</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4313</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4322</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4323</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4324</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4325</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4335</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4338</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4367</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4392</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="936" ind1="b" ind2="k"><subfield code="a">56.00</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">6</subfield><subfield code="j">2014</subfield><subfield code="e">1</subfield><subfield code="b">21</subfield><subfield code="c">01</subfield></datafield></record></collection>
author	Srinivasa, Chikkol V
spellingShingle	Srinivasa, Chikkol V ddc 620 bkl 56.00 misc Cylindrical skew panel misc Panel angle misc Skew angle misc Fiber orientation angle misc Antisymmetric laminate misc Finite element analysis misc Natural frequency Experimental and finite element studies on free vibration of cylindrical skew panels
authorStr	Srinivasa, Chikkol V
ppnlink_with_tag_str_mv	@@773@@(DE-627)684551314
format	electronic Article
dewey-ones	620 - Engineering & allied operations 690 - Buildings
delete_txt_mv	keep
author_role	aut aut aut
collection	springer
remote_str	true
illustrated	Not Illustrated
issn	2008-6695
topic_title	620 690 ASE 56.00 bkl Experimental and finite element studies on free vibration of cylindrical skew panels Cylindrical skew panel (dpeaa)DE-He213 Panel angle (dpeaa)DE-He213 Skew angle (dpeaa)DE-He213 Fiber orientation angle (dpeaa)DE-He213 Antisymmetric laminate (dpeaa)DE-He213 Finite element analysis (dpeaa)DE-He213 Natural frequency (dpeaa)DE-He213
topic	ddc 620 bkl 56.00 misc Cylindrical skew panel misc Panel angle misc Skew angle misc Fiber orientation angle misc Antisymmetric laminate misc Finite element analysis misc Natural frequency
topic_unstemmed	ddc 620 bkl 56.00 misc Cylindrical skew panel misc Panel angle misc Skew angle misc Fiber orientation angle misc Antisymmetric laminate misc Finite element analysis misc Natural frequency
topic_browse	ddc 620 bkl 56.00 misc Cylindrical skew panel misc Panel angle misc Skew angle misc Fiber orientation angle misc Antisymmetric laminate misc Finite element analysis misc Natural frequency
format_facet	Elektronische Aufsätze Aufsätze Elektronische Ressource
format_main_str_mv	Text Zeitschrift/Artikel
carriertype_str_mv	cr
hierarchy_parent_title	International journal of advanced structural engineering
hierarchy_parent_id	684551314
dewey-tens	620 - Engineering 690 - Building & construction
hierarchy_top_title	International journal of advanced structural engineering
isfreeaccess_txt	true
familylinks_str_mv	(DE-627)684551314 (DE-600)2649231-3
title	Experimental and finite element studies on free vibration of cylindrical skew panels
ctrlnum	(DE-627)SPR032822421 (SPR)2008-6695-6-1-e
title_full	Experimental and finite element studies on free vibration of cylindrical skew panels
author_sort	Srinivasa, Chikkol V
journal	International journal of advanced structural engineering
journalStr	International journal of advanced structural engineering
lang_code	eng
isOA_bool	true
dewey-hundreds	600 - Technology
recordtype	marc
publishDateSort	2014
contenttype_str_mv	txt
author_browse	Srinivasa, Chikkol V Suresh, Yalaburgi J Prema kumar, Wooday P
container_volume	6
class	620 690 ASE 56.00 bkl
format_se	Elektronische Aufsätze
author-letter	Srinivasa, Chikkol V
doi_str_mv	10.1186/2008-6695-6-1
dewey-full	620 690
author2-role	verfasserin
title_sort	experimental and finite element studies on free vibration of cylindrical skew panels
title_auth	Experimental and finite element studies on free vibration of cylindrical skew panels
abstract	Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels.
abstractGer	Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels.
abstract_unstemmed	Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels.
collection_details	GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_2027 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4392 GBV_ILN_4700
container_issue	1
title_short	Experimental and finite element studies on free vibration of cylindrical skew panels
url	https://dx.doi.org/10.1186/2008-6695-6-1
remote_bool	true
author2	Suresh, Yalaburgi J Prema kumar, Wooday P
author2Str	Suresh, Yalaburgi J Prema kumar, Wooday P
ppnlink	684551314
mediatype_str_mv	c
isOA_txt	true
hochschulschrift_bool	false
doi_str	10.1186/2008-6695-6-1
up_date	2024-07-03T14:58:05.944Z
_version_	1803570313634512896
fullrecord_marcxml	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">SPR032822421</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20220111205428.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">201007s2014 xx \|\|\|\|\|o 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1186/2008-6695-6-1</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)SPR032822421</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(SPR)2008-6695-6-1-e</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">620</subfield><subfield code="a">690</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">56.00</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Srinivasa, Chikkol V</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Experimental and finite element studies on free vibration of cylindrical skew panels</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2014</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The present paper deals with experimental and finite element studies carried out on free vibration of isotropic and laminated composite cylindrical skew panels. Natural frequencies were determined using CQUAD8 finite element of MSC Nastran, and comparison was made between the experimental values and the finite element solution. Effects of the skew angle and aspect ratio on the natural frequencies of isotropic cylindrical skew panels were studied. The effects of skew angle, aspect ratio, fiber orientation angle, and laminate stacking sequence (keeping total number of layers in the laminate constant) on the natural frequencies of antisymmetric laminated composite cylindrical skew panels were also studied. The experimental values of the first, second, and third natural frequencies are in good agreement with the finite element solution for both isotropic and laminated composite cylindrical panels. The first, second, and third natural frequencies are found to decrease with the increase in the aspect ratio for both isotropic and laminated composite cylindrical panels.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Cylindrical skew panel</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Panel angle</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Skew angle</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Fiber orientation angle</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Antisymmetric laminate</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Finite element analysis</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Natural frequency</subfield><subfield code="7">(dpeaa)DE-He213</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Suresh, Yalaburgi J</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Prema kumar, Wooday P</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">International journal of advanced structural engineering</subfield><subfield code="d">Berlin : Springer, 2009</subfield><subfield code="g">6(2014), 1 vom: 21. Jan.</subfield><subfield code="w">(DE-627)684551314</subfield><subfield code="w">(DE-600)2649231-3</subfield><subfield code="x">2008-6695</subfield><subfield code="7">nnns</subfield></datafield><datafield tag="773" ind1="1" ind2="8"><subfield code="g">volume:6</subfield><subfield code="g">year:2014</subfield><subfield code="g">number:1</subfield><subfield code="g">day:21</subfield><subfield code="g">month:01</subfield></datafield><datafield tag="856" ind1="4" ind2="0"><subfield code="u">https://dx.doi.org/10.1186/2008-6695-6-1</subfield><subfield code="z">kostenfrei</subfield><subfield code="3">Volltext</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_USEFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">SYSFLAG_A</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_SPRINGER</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_20</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_22</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_23</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_24</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_31</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_39</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_40</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_60</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_62</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_63</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_65</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_69</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_70</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_73</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_95</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_105</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_110</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_151</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_161</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_170</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_213</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_230</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_285</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_293</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_370</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_602</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2014</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_2027</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4012</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4037</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4112</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4125</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4126</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4249</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4305</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4306</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4307</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4313</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4322</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4323</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4324</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4325</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4335</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4338</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4367</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4392</subfield></datafield><datafield tag="912" ind1=" " ind2=" "><subfield code="a">GBV_ILN_4700</subfield></datafield><datafield tag="936" ind1="b" ind2="k"><subfield code="a">56.00</subfield><subfield code="q">ASE</subfield></datafield><datafield tag="951" ind1=" " ind2=" "><subfield code="a">AR</subfield></datafield><datafield tag="952" ind1=" " ind2=" "><subfield code="d">6</subfield><subfield code="j">2014</subfield><subfield code="e">1</subfield><subfield code="b">21</subfield><subfield code="c">01</subfield></datafield></record></collection>
score	7.401531

Nicht das Richtige dabei?

Schreiben Sie uns!

Experimental and finite element studies on free vibration of cylindrical skew panels

Nicht das Richtige dabei?

Zugang & Verfügbarkeit

Vorhandene Bände

Nicht das Richtige dabei?