The linearly stretching wall jet

It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable). Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Jafarimoghaddam, Amin [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2019

Schlagwörter:	The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow

Übergeordnetes Werk:	Enthalten in: European journal of mechanics / B - Paris : Gauthier-Villars, 1998, 80, Seite 52-59
Übergeordnetes Werk:	volume:80 ; pages:52-59

DOI / URN:	10.1016/j.euromechflu.2019.12.001

Katalog-ID:	ELV003642755

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245	1	0	\|a The linearly stretching wall jet
264		1	\|c 2019
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337			\|a Computermedien \|b c \|2 rdamedia
338			\|a Online-Ressource \|b cr \|2 rdacarrier
520			\|a It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable).
650		4	\|a The stretching wall jet
650		4	\|a Perturbation analysis
650		4	\|a Numerical solution
650		4	\|a Wall jet
650		4	\|a Stretching sheet
650		4	\|a Non-similar flow
773	0	8	\|i Enthalten in \|t European journal of mechanics / B \|d Paris : Gauthier-Villars, 1998 \|g 80, Seite 52-59 \|h Online-Ressource \|w (DE-627)320593878 \|w (DE-600)2019287-3 \|w (DE-576)114088284 \|x 1873-7390 \|7 nnns
773	1	8	\|g volume:80 \|g pages:52-59
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912			\|a GBV_ILN_110
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912			\|a GBV_ILN_2044
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912			\|a GBV_ILN_2061
912			\|a GBV_ILN_2064
912			\|a GBV_ILN_2065
912			\|a GBV_ILN_2068
912			\|a GBV_ILN_2088
912			\|a GBV_ILN_2111
912			\|a GBV_ILN_2112
912			\|a GBV_ILN_2113
912			\|a GBV_ILN_2118
912			\|a GBV_ILN_2122
912			\|a GBV_ILN_2129
912			\|a GBV_ILN_2143
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912			\|a GBV_ILN_2152
912			\|a GBV_ILN_2153
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912			\|a GBV_ILN_4037
912			\|a GBV_ILN_4112
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912			\|a GBV_ILN_4335
912			\|a GBV_ILN_4338
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936	b	k	\|a 50.33 \|j Technische Strömungsmechanik
951			\|a AR
952			\|d 80 \|h 52-59

Indexfelder

author_variant	a j aj
matchkey_str	article:18737390:2019----::hlnalsrthn
hierarchy_sort_str	2019
bklnumber	50.33
publishDate	2019
allfields	10.1016/j.euromechflu.2019.12.001 doi (DE-627)ELV003642755 (ELSEVIER)S0997-7546(19)30433-9 DE-627 ger DE-627 rda eng 530 DE-600 50.33 bkl Jafarimoghaddam, Amin verfasserin aut The linearly stretching wall jet 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable). The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow Enthalten in European journal of mechanics / B Paris : Gauthier-Villars, 1998 80, Seite 52-59 Online-Ressource (DE-627)320593878 (DE-600)2019287-3 (DE-576)114088284 1873-7390 nnns volume:80 pages:52-59 GBV_USEFLAG_U SYSFLAG_U GBV_ELV GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.33 Technische Strömungsmechanik AR 80 52-59
spelling	10.1016/j.euromechflu.2019.12.001 doi (DE-627)ELV003642755 (ELSEVIER)S0997-7546(19)30433-9 DE-627 ger DE-627 rda eng 530 DE-600 50.33 bkl Jafarimoghaddam, Amin verfasserin aut The linearly stretching wall jet 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable). The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow Enthalten in European journal of mechanics / B Paris : Gauthier-Villars, 1998 80, Seite 52-59 Online-Ressource (DE-627)320593878 (DE-600)2019287-3 (DE-576)114088284 1873-7390 nnns volume:80 pages:52-59 GBV_USEFLAG_U SYSFLAG_U GBV_ELV GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.33 Technische Strömungsmechanik AR 80 52-59
allfields_unstemmed	10.1016/j.euromechflu.2019.12.001 doi (DE-627)ELV003642755 (ELSEVIER)S0997-7546(19)30433-9 DE-627 ger DE-627 rda eng 530 DE-600 50.33 bkl Jafarimoghaddam, Amin verfasserin aut The linearly stretching wall jet 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable). The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow Enthalten in European journal of mechanics / B Paris : Gauthier-Villars, 1998 80, Seite 52-59 Online-Ressource (DE-627)320593878 (DE-600)2019287-3 (DE-576)114088284 1873-7390 nnns volume:80 pages:52-59 GBV_USEFLAG_U SYSFLAG_U GBV_ELV GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.33 Technische Strömungsmechanik AR 80 52-59
allfieldsGer	10.1016/j.euromechflu.2019.12.001 doi (DE-627)ELV003642755 (ELSEVIER)S0997-7546(19)30433-9 DE-627 ger DE-627 rda eng 530 DE-600 50.33 bkl Jafarimoghaddam, Amin verfasserin aut The linearly stretching wall jet 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable). The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow Enthalten in European journal of mechanics / B Paris : Gauthier-Villars, 1998 80, Seite 52-59 Online-Ressource (DE-627)320593878 (DE-600)2019287-3 (DE-576)114088284 1873-7390 nnns volume:80 pages:52-59 GBV_USEFLAG_U SYSFLAG_U GBV_ELV GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.33 Technische Strömungsmechanik AR 80 52-59
allfieldsSound	10.1016/j.euromechflu.2019.12.001 doi (DE-627)ELV003642755 (ELSEVIER)S0997-7546(19)30433-9 DE-627 ger DE-627 rda eng 530 DE-600 50.33 bkl Jafarimoghaddam, Amin verfasserin aut The linearly stretching wall jet 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable). The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow Enthalten in European journal of mechanics / B Paris : Gauthier-Villars, 1998 80, Seite 52-59 Online-Ressource (DE-627)320593878 (DE-600)2019287-3 (DE-576)114088284 1873-7390 nnns volume:80 pages:52-59 GBV_USEFLAG_U SYSFLAG_U GBV_ELV GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_101 GBV_ILN_105 GBV_ILN_110 GBV_ILN_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 50.33 Technische Strömungsmechanik AR 80 52-59
language	English
source	Enthalten in European journal of mechanics / B 80, Seite 52-59 volume:80 pages:52-59
sourceStr	Enthalten in European journal of mechanics / B 80, Seite 52-59 volume:80 pages:52-59
format_phy_str_mv	Article
bklname	Technische Strömungsmechanik
institution	findex.gbv.de
topic_facet	The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow
dewey-raw	530
isfreeaccess_bool	false
container_title	European journal of mechanics / B
authorswithroles_txt_mv	Jafarimoghaddam, Amin @@aut@@
publishDateDaySort_date	2019-01-01T00:00:00Z
hierarchy_top_id	320593878
dewey-sort	3530
id	ELV003642755
language_de	englisch
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author	Jafarimoghaddam, Amin
spellingShingle	Jafarimoghaddam, Amin ddc 530 bkl 50.33 misc The stretching wall jet misc Perturbation analysis misc Numerical solution misc Wall jet misc Stretching sheet misc Non-similar flow The linearly stretching wall jet
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topic_title	530 DE-600 50.33 bkl The linearly stretching wall jet The stretching wall jet Perturbation analysis Numerical solution Wall jet Stretching sheet Non-similar flow
topic	ddc 530 bkl 50.33 misc The stretching wall jet misc Perturbation analysis misc Numerical solution misc Wall jet misc Stretching sheet misc Non-similar flow
topic_unstemmed	ddc 530 bkl 50.33 misc The stretching wall jet misc Perturbation analysis misc Numerical solution misc Wall jet misc Stretching sheet misc Non-similar flow
topic_browse	ddc 530 bkl 50.33 misc The stretching wall jet misc Perturbation analysis misc Numerical solution misc Wall jet misc Stretching sheet misc Non-similar flow
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title	The linearly stretching wall jet
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title_full	The linearly stretching wall jet
author_sort	Jafarimoghaddam, Amin
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title_sort	the linearly stretching wall jet
title_auth	The linearly stretching wall jet
abstract	It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable).
abstractGer	It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable).
abstract_unstemmed	It is constructed a set-up comprising a jet from a slit at the leading edge, discharged over a linearly stretching wall. The non-similar flow can be interpreted as a combination of two distinct similarity regions; Akatnow–Glauert flow at the leading edge and Crane flow far away from it. In this respect, it is employed appropriate coordinate expansions to explore perturbatively the behavior of the flow near the similarity regions. A suitable composite transformation amalgamated with an abridgmentof the stream-wise coordinate, facilitated an immaculate numerical simulation of the involved nonlinear partial differential equation over the entire spatial domain ( 0 ≤ X < ∞ , 0 ≤ η ˆ < ∞ ) followed by quasi-linearization technique together with an implicit algorithm of a tridiagonal form. As a result, shear stress at the wall is accurately predicted through a proposed formulation, valid all the way along the wall. It is also exhibited that there exists a transition region with a critical coordinate in the stream-wise direction in which the shear stress at the wall becomes zero. This universal coordinate (namely, the turning point) is determined as, reasonably close to, X c r. ≈ 13 23 ( X is a dimensionless coordinate measuring distance along the wall and η ˆ is the dimensionless non-similarity variable).
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title_short	The linearly stretching wall jet
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up_date	2024-07-06T20:18:53.090Z
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