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Comparison of various drag coefficient expansions using polynomials and splinesThe longitudinal differential equation of motion has been used to investigate various aerodynamic expansion techniques. The total drag coefficient was expanded using conventional polynomials and splines with and without floating knot locations. This paper discusses the various techniques and approaches, compares results obtained from simultaneously fitting four separate flights (time vs distance measurements) and outlines the potential advantages and/or disadvantages of the various aerodynamic expansion techniques. It is believed that this is the first time splines have been used in the aerodynamic coefficient estimation process and that these results and techniques are germane to other applications.
Document ID
19840059571
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sabot, S. M.
(Air Force Armament Lab. Eglin AFB, FL, United States)
Winchenbach, G. L.
(USAF, Armament Laboratory, Eglin AFB FL, United States)
Chapman, G. T.
(NASA Ames Research Center Thermo- and Gas Dynamics Div., Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 84-2113
Report Number: AIAA PAPER 84-2113
Accession Number
84A42358
Distribution Limits
Public
Copyright
Other

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