Closed-form approach to rocket-vehicles aeroelastic divergence-Reference-Cited by-同舟云学术

Closed-form approach to rocket-vehicles aeroelastic divergence

Published:1989-03 Issue:2 Volume:26 Page:95-102
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Elyada Dov¹

Affiliation:

1. Israel Armament Development Authority, Haifa, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.26038

Reference11 articles.

1. Thomson, K. D. "The Aero-Elastic Divergence of Slender Multistage Test Vehicles," Weapons Research Establishment, Salisbury, South Australia. TN HSA 93, Nov.1962.

2. Aeroelastic analysis of sounding rocket vehicles

3. Aeroelastic bending of a sounding rocket vehicle

4. General static aeroelastic analysis for a body of revolution.

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