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Historical trend in the research and development of aircraftResults are presented from a study of aircraft design trends undertaken to determine the relationship between research, development, test and evaluation and aircraft mission capability, requirements and objectives. It is shown that while in some cases a performance objective was the primary research driver, research was the driver in the formulation of objectives in others. Among the topics discussed are: (1) speed considerations such as compressibility, propulsion and test techniques; (2) airframe considerations such as swept, delta, trapezoidal and variable-sweep planforms and mission commonality; (3) research aircraft; (4) the recent impact of computer-aided design; (5) Soviet aircraft development approaches and (6) a comparison of Soviet and U.S. military aircraft design trends. Attention is given to experimental and prototype aircraft programs which, although cancelled, anticipated significant subsequent developments.
Document ID
19810059530
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 11, 2013
Publication Date
August 1, 1981
Subject Category
Aeronautics (General)
Report/Patent Number
AIAA PAPER 81-1613
Meeting Information
Meeting: Aircraft Systems and Technology Conference
Location: Dayton, OH
Start Date: August 11, 1981
End Date: August 13, 1981
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
81A43934
Distribution Limits
Public
Copyright
Other

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