Effects of Double-Wedge Aft Angle on Hypersonic Laminar Flows
Author:
Affiliation:
1. Samsun University, 55420 Samsun, Turkey
2. Istanbul Technical University, 34469 Istanbul, Turkey
Funder
National Center of High Performance Computing of Turkey
TUBITAK
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference38 articles.
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2. EdneyB., Anomalous Heat Transfer and Pressure Distributions on Blunt Bodies at Hypersonic Speeds in the Presence of an Impinging Shock, Flygtekniska försöksanstalten, Stockholm, 1968, pp. 5–61.
3. Application of PIV in a Mach 7 double-ramp flow
4. Flowfield Establishment in Hypervelocity Shock-Wave/Boundary-Layer Interactions
5. Investigation of the separated region ahead of three-dimensional protuberances on plates and cones in hypersonic flows with laminar boundary layers
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