TY  - RPRT
TI  - Four-Nozzle Benchmark Wind Tunnel Model USA Code Solutions for Simulation of Multiple Rocket Base Flow Recirculation at 145,000 Feet Altitude
AU  - Dougherty, N. S.
AU  - Johnson, S. L.
PY  - 1993
UR  - https://ntrs.nasa.gov/citations/19950017234
ID  - 19950017234
ER  -