TY  - RPRT
TI  - A system for aerodynamic design and analysis of supersonic aircraft. Part 3: Computer program description
AU  - Middleton, W. D.
AU  - Lundry, J. L.
AU  - Coleman, R. G.
PY  - 1980
UR  - https://ntrs.nasa.gov/citations/19810006456
ID  - 19810006456
ER  -