TY  - RPRT
TI  - Hypersonic research engine project. Phase 2: Aerothermodynamic Integration Model (AIM) test report
AU  - Andersen, W. L.
AU  - Kado, L.
PY  - 1975
UR  - https://ntrs.nasa.gov/citations/19750018941
ID  - 19750018941
ER  -