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Historical development of worldwide supersonic aircraftAerodynamic 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.
Document ID
19790063882
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Spearman, M. L.
(NASA Langley Research Center Aeronautical Systems Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
August 1, 1979
Subject Category
Aeronautics (General)
Report/Patent Number
AIAA PAPER 79-1815
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Aircraft Systems and Technology Meeting
Location: New York, NY
Start Date: August 20, 1979
End Date: August 22, 1979
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
79A47895
Distribution Limits
Public
Copyright
Other

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