Correlation of hypersonic stagnation point heat transfer at low Reynolds numbers
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8296
Reference13 articles.
1. Aerodynamic Heating of Simple Geometries in the Slip - and Intermediate - Flow Regimes
2. AERODYNAMIC COEFFICIENTS IN THE SLIP AND TRANSITION REGIME
3. Experimental Effect of Bluntness and Gas Rarefaction on Drag Coefficients and Stagnation Heat Transfer on Axisymmetric Shapes in Hypersonic Flow
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