Dissociative cooling - Effect on stagnation heat transfer of gas mixture injection
Author:
Affiliation:
1. University of Texas at Austin, Austin, Texas 78712
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26683
Reference27 articles.
1. ^eshotko, E., and Cohen, C, "Heat Transfer at the Forward Stagnation Point of Blunt Bodies," NACA TN 3513,1955.
2. The Homogeneous Boundary Layer at an Axisymmetric Stagnation Point With Large Rates of Injection
3. Mass Transfer Cooling in a Boundary Layer
4. The Effect of Diffusion Thermo and Thermal Diffusion for Helium Injection Into Plane and Axisymmetric Stagnation Flow of Air
5. Helium Injection Into the Boundary Layer at an Axisymmetric Stagnation Point
Cited by 2 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. Heat transfer—a review of 1995 literature;International Journal of Heat and Mass Transfer;1999-08
2. Unsteady Effects of Dissociative Cooling Under High-Stagnation-Point Heat Loads;Journal of Spacecraft and Rockets;1998-09
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