1. The computationalanalysiswas performed using the inviscid AR0-111 and viscous MISSBLlO codes. The method used to couple the viscous and inviscid solutions involved obtaining an inviscid solution with the Euler solver (ARO-1) and then using the computed velocity distribution associated with the cells immediately adjacent to the missile surface as input into the viscous code (MISSBL); no additional interaction was involved.
2. 7 - 0 . 5 L t ' ' ' '
3. of high-area-ratio nozzle exhaust expanding into near vacuum. 0,MO0.m5 - o.mo-0.025 - 0.020- Catculatd 0.015 - 0.010 - n m .