A NUMERICALLY EFFICIENT FINITE ELEMENT HYDROELASTIC ANALYSIS
Author:
Affiliation:
1. THE AEROSPACE CORPORATION, EL SEGUNDO, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1976-1533
Reference15 articles.
1. "Prevention of Coupled Structure - Propulsion Instability (POGO), NASA SP-8055, October 1970.
2. Pinson, L. D. and C. G. Brown, "A Finite Element Method for Nonaxisymmetric Vibrations of Pressurized Shells of Revolution Partially Filled with Liquid, AIAA Paper No. 73-399, March 1973.
3. Palmer, J.H. and G. W. Asher, "Calculation of Axisymmetric Longitudinal Modes for Fluid-Elastic Tank-Ullage Gas Systems and Comparison with Model Test Results, I' AIAA Symposium on Structural Dynamics and Aeroelasticity, Aug. 30-Sept. 1, 1965, pp. 189-193.
4. Guyan, R. J, "Study on Dynamics of an Ellipsoidal Bulkhead Containing Fluid, I' Rockwell International, Space Div., Tech. Summary Report SD71-183, Sept. 1971.
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