Measurements of Stagnation Point Heat Transfer at Low Reynolds Numbers
Author:
Affiliation:
1. Polytechnic Institute of Brooklyn,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.9617
Reference6 articles.
Cited by 23 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. Aerobrake heating rate sensitivity study for the Aeroassist Flight Experiment (AFE);24th Thermophysics Conference;1989-06-12
2. Investigation of hypersonic three-dimensional flow past blunt bodies within the framework of the parabolized Navier-Stokes equations;Fluid Dynamics;1988
3. Comparison of viscous shock layer and boundary layer reentry heatingtechniques for Orbiter nose cap;4th Thermophysics and Heat Transfer Conference;1986-06-02
4. Hypersonic Merged Stagnation Shock Layers Part 11: Cold Wall Case;AIAA Journal;1974-03
5. Experimental investigations of local heat fluxes on a sphere and on the spherical blunt end of an axisymmetric body;Fluid Dynamics;1973
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