Experimental investigation of panel divergence at subsonic speeds
Author:
Affiliation:
1. Dartmouth College, Hanover, N. H.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6495
Reference9 articles.
1. Aeroelastic instabilities of simply supported panels in subsonic flow
2. SUBSONIC FLUTTER OF PANELS ON CONTINUOUS ELASTIC FOUNDATIONS
3. Ventres, C. S. "Nonlinear Flutter of Clamped Plates," Ph.D. thesis,Oct. 1969, Princeton Univ., Princeton, N. J.
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