TY  - RPRT
TI  - Inlet Development for a Rocket Based Combined Cycle, Single Stage to Orbit Vehicle Using Computational Fluid Dynamics
AU  - DeBonis, J. R.
AU  - Trefny, C. J.
AU  - Steffen, C. J., Jr.
PY  - 1999
UR  - https://ntrs.nasa.gov/citations/19990062664
ID  - 19990062664
ER  -