Flight Test Base Pressure Results at Hypersonic Mach Numbers in Turbulent Flow
Author:
Affiliation:
1. General Electric Company, King of Prussia, Pa.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.50095
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1. A Study of Creep Collapse of a Long Circular Cylindrical Shell Under Uniform External Pressure
2. Kriechfestigkeit metallischer Werkstoffe
3. Kriechknicken bei ver�nderlicher Axiallast
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