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Applications of dynamic stability parameters to problems in aircraft dynamicsThe application and analysis of dynamic stability parameters were examined. The effects of wing leading edge modifications on the stalling and spinning characteristics of a single engine general aviation research airplane are evaluated. It is illustrated how dynamic stability parameters measured in wind tunnel tests are used to predict the spin resistance of this class of aircraft, and that autorotation criteria are derived from the relationships which exist between static and dynamic aerodynamic characteristics.
Document ID
19810022580
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chambers, J. R. (NASA Langley Research Center Hampton, VA, United States)
Dicarlo, D. J. (NASA Langley Research Center Hampton, VA, United States)
Johnson, J. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 11, 2013
Publication Date
May 1, 1981
Publication Information
Publication: AGARD Dyn. Stability Parameters
Subject Category
Instrumentation And Photography
Accession Number
81N31122
Distribution Limits
Public
Copyright
Other
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