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Methods of obtaining stability derivativesVarious methods of obtaining aerodynamic derivatives are reviewed. These methods include wind-tunnel tests, aerodynamic theory, and extraction from flight tests, with the emphasis being on flight tests. Two techniques for extracting derivatives from flight are covered in sufficient detail to indicate the procedures involved. These methods are a strict least-squares approach and an iteration technique. References are listed for additional background and details of various techniques.
Document ID
19710015227
Acquisition Source
Legacy CDMS
Document Type
Contribution to a larger work
Authors
M. J. Queijo
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1971
Publication Information
Publication: Performance and Dynamics of Aerospace Vehicles
Publisher: National Aeronautics and Space Administration
Volume: SP-258
Issue Publication Date: January 1, 1971
URL: https://ntrs.nasa.gov/citations/19710015225
Subject Category
Aerodynamics
Accession Number
71N24703
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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