The effects of shock wave precursors ahead of hypersonic entry vehicles-Reference-Cited by-同舟云学术

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The effects of shock wave precursors ahead of hypersonic entry vehicles

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference
language:
Short-container-title:

Author:

STANLEY SCOTT¹,CARLSON LELAND¹

Affiliation:

1. Texas A & M University, College Station

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1465

Reference31 articles.

1. PolytechnicInstitute,Blacksburg,VA,Mdch 1968.

2. andatEarth", AIAAPaper 90-0052,Jan. 1990.

3. Tiwari,S.N., and Szema,K.Y."EffectsofPrecursor HeatingonChemicalandRadiativeNonequilibrium ViscousFlowAroundaJovianEntryBody",AIAA Paper 78-907,May 1978.

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. Full Three-Dimensional Monte Carlo Radiative Transport for Hypersonic Entry Vehicles;Journal of Spacecraft and Rockets;2019-01

2. Coupled radiation effects in thermochemical nonequilibrium shock-capturing flowfield calculations;27th Thermophysics Conference;1992-07-06

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