Mass transfer and first-order boundary-layer effects on sharp cone drag. II - At hypersonic conditions.
Author:
Affiliation:
1. ARO Inc., Arnold Air Force Station, Tenn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.3824
Reference12 articles.
1. Laminar heat transfer to spherically blunted cones at hypersonic conditions
2. Hypersonic viscous drag effects on blunt slender cones
3. HYPERSONIC FLOW OVER A SLENDER CONE WITH GAS INJECTION
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1. Second-order boundary-layer flow past sharp cones;International Journal of Heat and Mass Transfer;1983-10
2. Hypersonic viscous static stability of a sharp 5-deg cone at incidence;AIAA Journal;1976-08
3. Effect of gaseous injection on the hypersonic flow around transpiration-cooled bodies.;Journal of Spacecraft and Rockets;1969-06
4. Binary boundary layers on sharp cones in low-density supersonic and hypersonic flow.;AIAA Journal;1969-04
5. Correlation of mass injection drag data for slender cones at hypersonic speeds.;AIAA Journal;1969-03
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