Similarity solutions for oscillating pointed-nose slender axisymmetric bodies — part I: circular cones-Reference-Cited by-同舟云学术

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Similarity solutions for oscillating pointed-nose slender axisymmetric bodies — part I: circular cones

Published:1999-07 Issue:2 Volume:45 Page:75-83
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Hemdan Hamdi T.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference19 articles.

1. Unsteady Newton–Busemann flow theory, Part I: airfoils;Hui;AIAA J.,1981

2. Unsteady Newton–Busemann Flow theory. Part III: frequency dependence and indicial response;Hui;Aeronaut. Q.,1982

3. Unsteady Newtonian flow over two-dimensional airfoils;Hemdan;Trans. Jap. Soc. Aeronaut. Space Sci.,1987

4. Dynamic stability of oscillating two-dimensional supersonic airfoils;Hemdan;Aerotec. Missili Spazio,1986

5. Newtonian flow over oscillating two-dimensional airfoils at moderate or large incidence;Hemdan;AIAA J.,1990

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