A theoretical and experimental investigation has been conducted to evaluate the fundamental supersonic aerodynamic characteristics of a generic twin-body wind-tunnel model. The experimental testing was performed in the Langley Unitary Plan Wind Tunnel at a Mach number of 2. 70. Experimental data were obtained on a simple rectangular-wing twin-body wind-tunnel model; these data were used to evaluate prediction methods and to investigate interference effects.
|Original language||English (US)|
|Journal||NASA Technical Paper|
|State||Published - Jan 1 1983|
All Science Journal Classification (ASJC) codes
- Aerospace Engineering