Viscous slipstream flow downstream of triple shock wave intersection in supersonic diffuser air flow, using Pitot and static pressure probe measurements
Viscous slipstream flow downstream of a centerline Mach reflection
1971-10-01
Miscellaneous
No indication
English
Propeller slipstream wing interactions at Mach no. 0.8
NTRS | 1978
|Propeller Slipstream Wing Interactions at Mach No. 0.8
SAE Technical Papers | 1978
|