Nacelle Integration to Reduce the Sonic Boom of Aircraft Designed to Cruise at Supersonic SpeedsReport as inadecuate



 Nacelle Integration to Reduce the Sonic Boom of Aircraft Designed to Cruise at Supersonic Speeds


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An empirical method for integrating the engine nacelles on a wing-fuselage-fin(s) configuration has been described. This method is based on Whitham theory and Seebass and George sonic-boom minimization theory, With it, both reduced sonic-boom as well as high aerodynamic efficiency methods can be applied to the conceptual design of a supersonic-crui

Author: Mack, Robert J

Source: https://archive.org/







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