A conformal mapping method to predict low-speed aerodynamic characteristics of arbitrary slender re-entry shapes.-Reference-Cited by-同舟云学术

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A conformal mapping method to predict low-speed aerodynamic characteristics of arbitrary slender re-entry shapes.

Published:1966-02 Issue:2 Volume:3 Page:247-253
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

SKULSKY ROBERT S.¹

Affiliation:

1. United Aircraft Corporation, Redondo Beach, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.28427

Reference14 articles.

1. Munk, M. M. "The aerodynamic forces on airship hulls/' NACARept. 184(1924).

2. Jones, R. T. "Properties of low-aspect-ratio pointed wings at speeds below and above the speed of sound," NACA Rept. 835(1946).

3. Heaslet, M. A., Lomax, H., and Spreiter, J. R. "Linearized compressible-flow theory for sonic flight speeds," NACA Rept. 956(1950).

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