Pressure data are presented in tabular form on the lower wing surface of the space shuttle launch vehicle configuration model. For Vol. III, see .
Airloads Investigation of an 0.30-Scale Model of the Space Shuttle Vehicle 140A/B Launch Configuration (Model 47-Ots) in the Arc 11-Foot Unitary Plan Wind Tunnel for Mach Range 0.6 to 1.4 (Ia14a), Volume 5
1975
957 pages
Report
No indication
English