NASA NTRS · 19750010114
Aerodynamic design and analysis system for supersonic aircraft. Part 3: Computer program description
Abstract
The computer program for the design and analysis of supersonic aircraft configurations is presented. The schematics of the program structure are provided. The individual overlays and subroutines are described. The system is useful in determining surface pressures and supersonic area rule concepts.
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Middleton, W. D., Lundry, J. L., Coleman, R. G.. 1975-03-01. Aerodynamic design and analysis system for supersonic aircraft. Part 3: Computer program description. https://ntrs.nasa.gov/citations/19750010114
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