Technical Papers
Sep 2, 2014

Improvement of the Newtonian Method to Estimate Supersonic Vehicle Drag

Publication: Journal of Aerospace Engineering
Volume 28, Issue 5

Abstract

A simple, easy-to-use method to compute vehicle drag at low and moderate supersonic speeds is presented in this study. A novel version of the Newtonian sine-squared law is proposed and used to compute supersonic pressure or wave drag for various geometries. The new version implicitly includes shockwave contribution not present in the original law. The results obtained are compared with the those found in the literature and discussed in order to estimate the applicability and validity of the method. The method’s suitability for optimization purposes is also briefly considered.

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Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 28Issue 5September 2015

History

Received: Apr 16, 2014
Accepted: Jul 16, 2014
Published online: Sep 2, 2014
Discussion open until: Feb 2, 2015
Published in print: Sep 1, 2015

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Authors

Affiliations

Timo Sailaranta [email protected]
Researcher, Dept. of Applied Mechanics, Aalto Univ., P.O. Box 14400, FI-00076 Aalto, Finland; and CEO, Aero RD Ltd., Otakuja 3, FI-02150 Espoo, Finland (corresponding author). E-mail: [email protected]
Tomi Honkanen [email protected]
Researcher, Dept. of Applied Mechanics, Aalto Univ., P.O. Box 14400, FI-00076 Aalto, Finland. E-mail: [email protected]
Ari Siltavuori [email protected]
Vice President, Aero RD Ltd., Otakuja 3, FI-02150 Espoo, Finland. E-mail: [email protected]

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