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There are a total of 27 record(s) matching your query.
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Results of an investigation of the space shuttle integrated vehicle aerodynamic heating characteristics obtained using the 0.0175-scale model 60-OTS in AEDC tunnel A during tests IH41B, volume 1
Author(s): Dye, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1977
Added to NTRS: 2005-10-13
Accession Number: 77N83628; Document ID: 19770082406; Report Number: DMS-DR-2295-VOL-1, NASA-CR-151069
Results of heat transfer tests on a 0.0175-scale space shuttle orbiter model (56-0) in the AEDC VKF 'B' Hypersonic Wind Tunnel (OH74)
Author(s): Dye, W. H.
Abstract: The results are presented of aerodynamic heating tests conducted on a 0.0175-scale model of the space shuttle orbiter. The tests were conducted at a nominal Mach number of 8 and model angles of attack varying between 20 deg ...
NASA Center: NASA (non Center Specific)
Publication Year: 1976
Added to NTRS: 2005-08-25
Accession Number: 76N21266; Document ID: 19760014178; Report Number: DMS-DR-2263, NASA-CR-144596
Results of test OH69 obtained in the AEDC VKF hypersonic tunnel B using the infrared scanning method to obtain heat transfer data on the 0.040 scale model 82-0 of the space shuttle forebody, volume 1
Author(s): Martinez, J. C.; Dye, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1978
Added to NTRS: 2005-08-25
Accession Number: 78N78066; Document ID: 19780078073; Report Number: DMS-DR-2321-VOL-1, NASA-CR-151410
Results of an investigation of the Space Shuttle Integrated Vehicle aerodynamic heating characteristics obtained using the 0.0175-scale model 60-OTS in AEDC Tunnel A during tests IH41B, volume 4
Author(s): Dye, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1977
Added to NTRS: 2004-11-03
Accession Number: 77N84214; Document ID: 19770082992; Report Number: DMS-DR-2295-VOL-4, NASA-CR-151072
Aerodynamic heating results obtained during test OH50B conducted in the AEDC VKF tunnel B using the 0.040-scale model 83-0 of the space shuttle orbiter forward fifty percent fuselage
Author(s): Dye, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1977
Added to NTRS: 2004-11-03
Accession Number: 77N79921; Document ID: 19770078699; Report Number: DMS-DR-2358, NASA-CR-151067
Report of pressure distribution tests of the 0.010-scale space shuttle vehicle 139 model (26-OTS) in the NASA/ARC 3.5-foot hypersonic wind tunnel (tests OH10 and IH2)
Author(s): Dye, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1981
Added to NTRS: 2004-11-03
Accession Number: 82N71292; Document ID: 19820066024; Report Number: DMS-DR-2085, NASA-CR-167344
Results of an investigation of the Space Shuttle Integrated Vehicle aerodynamic heating characteristics obtained using the 0.0175-scale model 60-OTS in AEDC Tunnel A during tests IH41B, volume 5
Author(s): Dye, W. H.
Abstract: No Abstract Available
NASA Center: NASA (non Center Specific)
Publication Year: 1977
Added to NTRS: 2004-11-03
Accession Number: 77N84215; Document ID: 19770082993; Report Number: DMS-DR-2295-VOL-5, NASA-CR-151073
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