Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection

Gespeichert in:

Autor*in:	Antonov, V. A. [verfasserIn] Grishin, A. M. [verfasserIn] Pakhomov, F. M. [verfasserIn]

Format:	Artikel
Sprache:	Englisch

Erschienen:	1987

Schlagwörter:	Flow Pattern Pressure Distribution Surface Pressure Stagnation Point Supersonic Flow

Übergeordnetes Werk:	Enthalten in: Fluid dynamics - New York, NY : Kluwer Acad./Consultants Bureau, 1967, 22(1987), 5 vom: Sept., Seite 737-742
Übergeordnetes Werk:	volume:22 ; year:1987 ; number:5 ; month:09 ; pages:737-742

Links:	Volltext

DOI / URN:	10.1007/BF01051695

Katalog-ID:	OLC203840352X

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allfieldsGer	10.1007/BF01051695 doi (DE-627)OLC203840352X (DE-He213)BF01051695-p DE-627 ger DE-627 rakwb eng 530 AVZ Antonov, V. A. verfasserin aut Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection 1987 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Flow Pattern (dpeaa)DE-He213 Pressure Distribution (dpeaa)DE-He213 Surface Pressure (dpeaa)DE-He213 Stagnation Point (dpeaa)DE-He213 Supersonic Flow (dpeaa)DE-He213 Grishin, A. M. verfasserin aut Pakhomov, F. M. verfasserin aut Enthalten in Fluid dynamics New York, NY : Kluwer Acad./Consultants Bureau, 1967 22(1987), 5 vom: Sept., Seite 737-742 (DE-627)129594172 (DE-600)240500-3 (DE-576)015087034 0015-4628 nnns volume:22 year:1987 number:5 month:09 pages:737-742 https://doi.org/10.1007/BF01051695 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_11 GBV_ILN_40 GBV_ILN_70 GBV_ILN_2014 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4309 GBV_ILN_4700 AR 22 1987 5 09 737-742
allfieldsSound	10.1007/BF01051695 doi (DE-627)OLC203840352X (DE-He213)BF01051695-p DE-627 ger DE-627 rakwb eng 530 AVZ Antonov, V. A. verfasserin aut Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection 1987 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier Flow Pattern (dpeaa)DE-He213 Pressure Distribution (dpeaa)DE-He213 Surface Pressure (dpeaa)DE-He213 Stagnation Point (dpeaa)DE-He213 Supersonic Flow (dpeaa)DE-He213 Grishin, A. M. verfasserin aut Pakhomov, F. M. verfasserin aut Enthalten in Fluid dynamics New York, NY : Kluwer Acad./Consultants Bureau, 1967 22(1987), 5 vom: Sept., Seite 737-742 (DE-627)129594172 (DE-600)240500-3 (DE-576)015087034 0015-4628 nnns volume:22 year:1987 number:5 month:09 pages:737-742 https://doi.org/10.1007/BF01051695 lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-TEC SSG-OLC-PHY GBV_ILN_11 GBV_ILN_40 GBV_ILN_70 GBV_ILN_2014 GBV_ILN_4046 GBV_ILN_4307 GBV_ILN_4309 GBV_ILN_4700 AR 22 1987 5 09 737-742
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author	Antonov, V. A.
spellingShingle	Antonov, V. A. ddc 530 misc Flow Pattern misc Pressure Distribution misc Surface Pressure misc Stagnation Point misc Supersonic Flow Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection
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Effect of angle of attack on supersonic flow past axisymmetric blunt bodies with surface injection

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