TY  - RPRT
TI  - Aerodynamic design and analysis system for supersonic aircraft. Part 3: Computer program description
AU  - Middleton, W. D.
AU  - Lundry, J. L.
AU  - Coleman, R. G.
PY  - 1975
UR  - https://ntrs.nasa.gov/citations/19750010114
ID  - 19750010114
ER  -