Aerodynamic problems in the development of supersonic aircraft, their solutions, and innovative design features are presented. Studies of compressibility, introduction of jets, supersonic phenomena, transonic drag and lift, longitudinal and directional stability, dynamic pressure fields, and advent of the supersonic fighter are discussed. The flight research aircraft such as the Bell X-1 and the Douglas-558, the century series models, reconnaissance aircraft, the multimission tactical fighter, and the current generation fighters such as F-16 and F-18 are described. The SCAT program is considered, along with supersonic developments in Great Britain, France, and USSR. It is concluded that the sonic boom still appears to be an inherent problem of supersonic flight that particularly affects overland commercial flight, and efforts continue for increased efficiency for economic and performance gains and increased safety for military and civilian aircraft.
Historical development of worldwide supersonic aircraft
American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting ; 1979 ; New York, NY
1979-08-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
Historical development of worldwide supersonic aircraft
AIAA | 1979
|Historical development of worldwide supersonic aircraft
NTRS | 1983
|Historical Development of Worldwide Supersonic Aircraft
NTIS | 1983
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NTIS | 1983
|Historical development of worldwide guided missiles
NTRS | 1983
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