Hydrogen Ionization in the Shock Layer for Entry into the Outer Planets

Author:

HOWE JOHN T.1

Affiliation:

1. NASA Ames Research Center, Moffett Field, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 13 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. Nonequilibrium Calculation of High-Temperature Radiating H2-He Flowfield;Journal of Thermophysics and Heat Transfer;2009-10

2. Stagnation-Region Heating Environment of the Galileo Probe;Journal of Thermophysics and Heat Transfer;2009-07

3. Coupled Rotational-Vibrational Relaxation of Molecular Hydrogen at High Temperatures;Journal of Thermophysics and Heat Transfer;2006-07

4. Calculation of H2-He Flow with Nonequilibrium Ionization and Radiation;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10

5. Heatshielding problems of planetary entry - A review;30th Fluid Dynamics Conference;1999-06-28

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