Heat-transfer measurements in a separated laminar base flow
Author:
Affiliation:
1. Sandia Laboratories, Albuquerque, N.Mex.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.27992
Reference13 articles.
1. An experimental investigation of the near wake of a slender cone at M infinity equal 8 and 12.
2. A study of laminar near wakes.
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Model for predicting hypersonic laminar near-wake flowfields;Journal of Spacecraft and Rockets;1996-03
2. Review and development of base pressure and base heating correlations in supersonic flow;Journal of Spacecraft and Rockets;1995-01
3. A survey of heat transfer in compressible separated and reattached flows;AIAA Journal;1988-02
4. Convective Heat Transfer Correlations for Planar, Supersonic, Separated Flows;Journal of Heat Transfer;1980-05-01
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