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Curved-flow, rolling-flow, and oscillatory pure-yawing wind-tunnel test methods for determination of dynamic stability derivativesDynamic stability derivatives are evaluated on the basis of rolling-flow, curved-flow and snaking tests. Attention is given to the hardware associated with curved-flow, rolling-flow and oscillatory pure-yawing wind-tunnel tests. It is found that the snaking technique, when combined with linear- and forced-oscillation methods, yields an important method for evaluating beta derivatives for current configurations at high angles of attack. Since the rolling flow model is fixed during testing, forced oscillations may be imparted to the model, permitting the measurement of damping and cross-derivatives. These results, when coupled with basic rolling-flow or rotary-balance data, yield a highly accurate mathematical model for studies of incipient spin and spin entry.
Document ID
19810042529
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Chambers, J. R.
(NASA Langley Research Center Hampton, VA, United States)
Grafton, S. B.
(NASA Langley Research Center Hampton, Va., United States)
Lutze, F. H.
(Virginia Polytechnic Institute and State University Blacksburg, Va., United States)
Date Acquired
August 11, 2013
Publication Date
March 1, 1981
Subject Category
Aircraft Stability And Control
Meeting Information
Meeting: Lecture Series on Dynamic Stability Parameters
Location: Moffett Field, CA
Country: US
Start Date: March 2, 1981
End Date: March 5, 1981
Sponsors: NATO, AGARD
Accession Number
81A26933
Distribution Limits
Public
Copyright
Other

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