Leading-edge bluntness effects in high enthalpy, hypersonic compression corner flow
Author:
Affiliation:
1. University of New South Wales, Canberra ACT 2600, Australia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.13392
Reference47 articles.
1. Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight Speeds
2. Perturbations of plane and axisymmetric entropy layers.
3. Wing leading-edge design concepts for airbreathing hypersonic waveriders
4. Boundary-layer displacement and leading-edge bluntness effects on attached and separated laminar boundary layers in a compression corner. II - Experimental study
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