An integrated system for the analysis of supersonic configurations consists of an executive driver and eight basic computer programs that build up force coefficients of an selected configuration. System employs modified linearized theory for calculation of surface pressures and employs supersonic-area-rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients.
Aerodynamics of Supersonic Aircraft
NASA Tech Briefs ; 6 , 2
1982-11-01
Miscellaneous
No indication
English
Aerodynamics of powerplant installation on supersonic aircraft
Engineering Index Backfile | 1967
|An Overview of Military Aircraft Supersonic Inlet Aerodynamics
British Library Conference Proceedings | 2012
|