Oscillating two-phase flow through a rigid pipe.
Author:
Affiliation:
1. Heliodyne Corporation, Van Nuys, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3804
Reference15 articles.
1. Moore, F. K. "Hypersonic boundary layer theory," Theory of Laminar Flows (Princeton University Press, Princeton, N.J., 1964), pp.439-527.
2. Newtonian Flow Theory for Slender Bodies
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