The Effect of an External Supersonic Flow on the Vibration Characteristics of Thin Cylindrical Shells
Author:
Affiliation:
1. Boeing Airplane Company,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.9264
Reference21 articles.
1. Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds
2. On the Vibration of Thin Cylindrical Shells Under Internal Pressure
3. Series A;Arnold R. N.,1949
4. Supersonic Flutter of a Cylindrical Shell
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