Thermally induced vibrations of long thin- walled cylinders of open section-Reference-Cited by-同舟云学术

Thermally induced vibrations of long thin- walled cylinders of open section

Published:1970-08 Issue:8 Volume:7 Page:897-905
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

FRISCH HAROLD P.¹

Affiliation:

1. NASA Goddard Space Flight Center, Greenbelt, Md.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.30068

Reference13 articles.

1. Proceedings of the Symposium on Gravity-Gradient Attitude Control, U.S. Air Force and Aerospace Corp., Dec. 1968, SAMSOTR-69-307, pp.3-1to 3-52 and 7-1 to7-17.

2. Timoshenko, S. "Theory of Bending, Torsion and Buckling of Thin Walled Members of Open Section/' Journal of the Franklin Institute, Vol.239, Nos. 3 and 4,1945, pp.201-219, 249-268.

3. Frisch, H. P. "Thermal Bending Plus Twist of a Thin-Walled Cylinder of Open Section With Application to Gravity-Gradient Booms/' TN D-4069, Aug. 1967, NASA.

4. An analytical representation of temperature distributions in gravitygradient rods.

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