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Results of a Landing Gear Loads Test Using a 0.0405-Scale Model (16-0) of the Space Shuttle Orbiter in the Rockwell International Naal Wind Tunnel (OA163), Volume 1

R. C. Mennell | NTIS | 1976

Keywords: Scale models , Wind tunnel models

Results of a Landing Gear Loads Test Using a 0.0405-Scale Model (16-0) of the Space Shuttle Orbiter in the Rockwell International Naal Wind Tunnel (OA163), Volume 3

R. C. Mennell | NTIS | 1976

Keywords: Scale models , Wind tunnel models

Results of a Landing Gear Loads Test Using a 0.0405-Scale Model (16-0) of the Space Shuttle Orbiter in the Rockwell International Naal Wind Tunnel (OA163), Volume 4

R. C. Mennell | NTIS | 1976

Keywords: Scale models , Wind tunnel models

Results of a Landing Gear Loads Test Using a 0.0405-Scale Model (16-0) of the Space Shuttle Orbiter in the Rockwell International Naal Wind Tunnel (OA163), Volume 2

R. C. Mennell | NTIS | 1976

Keywords: Scale models , Wind tunnel models

Results of an Investigation of Reynolds Effects on Integrated Vehicle Elevon Hinge Moments and Wing Panel Loads Obtained with 0.010 Scale Model 72 OTS in the Rockwell Trisonic Wind Tunnel (IA141)

R. C. Mennell | NTIS | 1976

Keywords: Scale models

Subsonic and Transonic Hinge Moment and Wing Bending/Torsion Characteristics of .015 Scale Space Shuttle Models 49-0 and 67-TS in the Rockwell International Trisonic Wind Tunnel (IA70), Volume 2

M. T. Hughes / R. C. Mennell | NTIS | 1974

Keywords: Scale models

Subsonic and Transonic Hinge Moment and Wing Bending/Torsion Characteristics of .015 Scale Space Shuttle Models 49-0 and 67-TS in the Rockwell International Trisonic Wind Tunnel (IA70), Volume 3

M. T. Hughes / R. C. Mennell | NTIS | 1974

Keywords: Scale models

Subsonic and Transonic Hinge Moment and Wing Bending/Torsion Characteristics of .015 Scale Space Shuttle Models 49-0 and 67-TS in the Rockwell International Trisonic Wind Tunnel (IA70), Volume 1

M. T. Hughes / R. C. Mennell | NTIS | 1974

Keywords: Scale models

Results of a Landing Gear Loads Test Using a 0.0405-Scale Model (16-0) of the Space Shuttle Orbiter in the Rockwell International Naal Wind Tunnel (Oa163b), Volume 2

R. C. Mennell | NTIS | 1977

Keywords: Scale models

Results of a Landing Gear Loads Test Using a 0.0405-Scale Model (16-0) of the Space Shuttle Orbiter in the Rockwell International Naal Wind Tunnel (Oa163b), Volume 1

R. C. Mennell | NTIS | 1977

Keywords: Scale models