NASA NTRS · 19960027894
A non-axisymmetric linearized supersonic wave drag analysis: Mathematical theory
Abstract
A Mathematical theory is developed to perform the calculations necessary to determine the wave drag for slender bodies of non-circular cross section. The derivations presented in this report are based on extensions to supersonic linearized small perturbation theory. A numerical scheme is presented utilizing Fourier decomposition to compute the pressure coefficient on and about a slender body of arbitrary cross section.
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Barnhart, Paul J.. 1996-05-01. A non-axisymmetric linearized supersonic wave drag analysis: Mathematical theory. https://ntrs.nasa.gov/citations/19960027894
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