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- W773536521 abstract "An integrated system of computer programs was developed for the design and analysis of supersonic configurations. The system uses linearized theory methods for the calculation of surface pressures and supersonic area rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients. Interactive graphics are optional at the user's request. Representative test cases and associated program output are presented." @default.
- W773536521 created "2016-06-24" @default.
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- W773536521 date "1980-12-01" @default.
- W773536521 modified "2023-09-23" @default.
- W773536521 title "A system for aerodynamic design and analysis of supersonic aircraft. Part 4: Test cases" @default.
- W773536521 hasPublicationYear "1980" @default.
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