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Requirement for simulation in V/STOL research aircraft programsThe application of flight simulation to aircraft design and development is discussed. The general stages of aircraft development are defined. The application of flight simulation to the following projects is reported: (1) the development and flight research of the Augmented Jet-Flap STOL research aircraft and (2) design studies of advanced VTOL research aircraft. It is stated that the simulation projects proved significant in helping establish criteria for the aircraft design and in facilitating the study of problems associated with new flight profiles, new methods of control, and special emergency conditions.
Document ID
19750005748
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Quigley, H. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Holzhauser, C. A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
October 1, 1974
Publication Information
Publication: AGARD V/STOL Aerodyn.
Subject Category
Aircraft Design, Testing And Performance
Accession Number
75N13820
Distribution Limits
Public
Copyright
Other
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