Comparisons of Air Radiation Model with Shock Tube Measurements-Reference-Cited by-同舟云学术

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Comparisons of Air Radiation Model with Shock Tube Measurements

Published:2009-01-05 Issue: Volume: Page:
ISSN:
Container-title:47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Bose Deepak¹,McCorkle Evan²,Bogdanoff David³,Allen Gary³

Affiliation:

1. NASA Ames Research Center

2. North Carolina State University

3. ELORET Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-1030

Reference12 articles.

1. Johnston, C.O. "Nonequilibrium Shock-Layer Radiative Heating for Earth and Titan Entry," Ph.D. Thesis,Virginia Polytechnic Institute andStateUniversity, Nov 2006.

2. RTO-AVT-VKI Lecture Series 2008.;Bogdanoff D.

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1. Survey of vacuum ultraviolet experimental data in relation to radiation characterization for Earth high-speed re-entry;The European Physical Journal D;2023-08

2. Advancements in the Modeling and Simulation of Shock Tube Flows;AIAA SCITECH 2022 Forum;2022-01-03

3. Scaling of Reflected Shock Bifurcation at High Incident Mach Number;AIAA AVIATION 2021 FORUM;2021-07-28

4. Measurement of Radiative Nonequilibrium for Air Shocks Between 7 and 9 km/s;Journal of Thermophysics and Heat Transfer;2020-01

5. Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography;AIAA Aviation 2019 Forum;2019-06-14

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