General static aeroelastic analysis for a body of revolution.-Reference-Cited by-同舟云学术

General static aeroelastic analysis for a body of revolution.

Published:1965-12 Issue:12 Volume:3 Page:2256-2261
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

O'KEEFE DAVID ALLEN¹

Affiliation:

1. Martin Company, Orlando, Fla.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.3354

Reference4 articles.

1. Bishlinghoff, R. L., Ashley, H., and Halfman, R. L., Aeroelasticity ( Addison-Wesley Publishing Company, Inc., Cambridge, Mass. 1955), Chap. II, pp.15-32.

2. Fimg, Y. C., An Introduction to the Theory of Aeroelasticity (John Wiley and Sons, Inc., New York, 1955), Chap. I, pp.19-27.

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1. References††The references are generally arranged alphabetically. However, for single-, double-, and multiple-author papers with the same first author, they are listed as follows:(i)the single-author papers first: e.g. SMITH, A. 1990 before SMITH, A. 1991;(ii)the double-author papers next, according to the second author’s name: e.g. SMITH, A. & BROWN, G. 1991 before SMITH, A. & GREEN, S. 1979;(iii)multiple-author papers, which will be cited in the text as, e.g. Smith et al. (1979), are listed last, strictly chronologically.§§All MERL Reports, e.g. Païdoussis & Denise (1970) are available on-line via: www.digital.library.mcgill.ca/pse/;Fluid-Structure Interactions;2016

2. Cylinders in Axial Flow I;Fluid-Structure Interactions;2016

3. Closed-form approach to rocket-vehicles aeroelastic divergence;Journal of Spacecraft and Rockets;1989-03

4. Static aeroelastic analysis of guided slender launch vehicles;Journal of Spacecraft and Rockets;1978-01

5. Recent advances in the estimation of sounding rocket structural loads;4th Sounding Rocket Technology Conference;1976-06-23