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US and USSR Military Aircraft and Missile Aerodynamics 1970-1980. A selected, annotated bibliography, volume 1The purpose of this selected bibliography (281 citations) is to list available, unclassified, unlimited publications which provide aerodynamic data on major aircraft and missiles currently used by the military forces of the United States of America and the Union of Soviet Socialist Republics. Technical disciplines surveyed include aerodynamic performance, static and dynamic stability, stall-spin, flutter, buffet, inlets nozzles, flap performance, and flying qualities. Concentration is on specific aircraft including fighters, bombers, helicopters, missiles, and some work on transports, which are or could be used for military purposes. The bibliography is limited to material published from 1970 to 1980. The publications herein illustrate many of the types of aerodynamic data obtained in the course of aircraft development programs and may therefore provide some guidance in identifying problems to be expected in the conduct of such work. As such, this information may be useful in planning future research programs.
Document ID
19810020581
Acquisition Source
Legacy CDMS
Document Type
Other - Other
Authors
Tuttle, M. H.
(NASA Langley Research Center Hampton, VA, United States)
Maddalon, D. V.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1981
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81951
L-14392
Report Number: NASA-TM-81951
Report Number: L-14392
Accession Number
81N29119
Funding Number(s)
PROJECT: RTOP 503-03-13-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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