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Role of research aircraft in technology developmentNASA supercritical wing technology, and the digital fly-by-wire program are discussed as used on the F-8 research aircraft. Furthermore, the Highly Maneuverable Aircraft Technology (HiMAT) program, using a 0.44-scale, 3500 lb jet-powered remotely piloted research aircraft, is analyzed. Highly accurate data on aerodynamic and structural loads and deflection data were obtained from model flight tests. In addition, an oblique-wing technology is discussed through the example of the piloted AD-1 research aircraft, noting the low cost of the experiment. Other topics include: integrated system technology; generic forces of the research aircraft program; and aeronautical technology application trends.
Document ID
19850033955
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Szalai, K. J.
(NASA Flight Research Center Research Engineering Div., Edwards, CA, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 84-2473
Accession Number
85A16106
Distribution Limits
Public
Copyright
Other

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