Combined compressive and shear buckling analysis of hypersonic aircraft sandwich panels-Reference-Cited by-同舟云学术

Combined compressive and shear buckling analysis of hypersonic aircraft sandwich panels

Published:1992-04-13 Issue: Volume: Page:
ISSN:
Container-title:33rd Structures, Structural Dynamics and Materials Conference
language:
Short-container-title:

Author:

KO WILLIAM¹,JACKSON RAYMOND¹

Affiliation:

1. NASA, Flight Research Center, Edwards, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2487

Reference23 articles.

1. 'Plank, P.P., I.F. Sakata, G.W. Davis, and C.C. Richie, Hypersonic Cruise Vehicle Wing Structure Evaluation, NASA CR-1568,1970.

2. Greene, Bruce E., Substantiation Data for Advanced Beaded and Tubular Structural Panels-Volume I, Design andAnalysis, NASA CR-132460,1974.

3. 3Musgrove,Max D., and Russell F. Northrop, SubstantiationDatafor Advanced Beaded and Tubular Structural Panels-Volume 2,Fabrication,NASACR-132482,1974.

4. Hedges,PhilipC., and BruceE.Greene,Substantiation Datafor Advanced Beaded and TubularStructural Panels-Volume3, Testing,NASA CR-132515, 1974.

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