Tabulated pressure data are presented on the left lower wing surface of a scale model of the integrated space shuttle vehicle configuration.
Results of a Pressure Loads Investigation on a 0.030-Scale Model (47-Ots) of the Integrated Space Shuttle Vehicle Configuration 5 in the NASA Ames Research Center 11 X 11 Foot Leg of the Unitary Plan Wind Tunnel (Ia81a), Volume 4
1975
730 pages
Report
No indication
English