Asymptotic behavior of hypersonic flow over blunted slender wedges.
Author:
Affiliation:
1. Institut fur Theoretische Gasdynamik der Deutschen Versuchsanstalt fur Luft- und Raumfahrt E.V., Aachen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4979
Reference12 articles.
1. Theory for Moderately Large Deflections of Thin Sandwich Shells
2. UNIRED THEORY FOR THE BENDING AND BUCKLING OF SANDWICH SHELLS - APPLICATION TO AXIALLY COMPRESSED CIRCULAR CYLINTRICAL SHELLS
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