Transition Experiments on Slightly Blunted Cones with Distributed Roughness in Hypersonic Flight
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California 94035-1000
2. ERC, Inc., Moffett Field, California 94035-1000
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J051616
Reference34 articles.
1. Correlation of Nosetip Boundary-Layer Transition Data Measured in Ballistics-Range Experiments
2. Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.
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4. Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds
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