TY  - RPRT
TI  - Hypersonic research engine project. Phase 2: Aerothermodynamic Integration Model (AIM) data reduction computer program, data item no. 54.16
AU  - Gaede, A. E.
AU  - Platte, W.
PY  - 1975
UR  - https://ntrs.nasa.gov/citations/19750019995
ID  - 19750019995
ER  -