NASA NTRS · 19840059571
Comparison of various drag coefficient expansions using polynomials and splines
Abstract
The 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.
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Sabot, S. M., Winchenbach, G. L., Chapman, G. T.. 1984-01-01. Comparison of various drag coefficient expansions using polynomials and splines. https://ntrs.nasa.gov/citations/19840059571
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