Wake flow calculations with ablation for the Stardust Sample Return Capsule-Reference-Cited by-同舟云学术

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Wake flow calculations with ablation for the Stardust Sample Return Capsule

Published:1997-06-23 Issue: Volume: Page:
ISSN:
Container-title:32nd Thermophysics Conference
language:
Short-container-title:

Author:

Olynick Dave¹,Chen Y.-K.¹,Tauber Michael¹,Olynick Dave¹,Chen Y.-K.¹,Tauber Michael¹

Affiliation:

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

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2477

Reference67 articles.

1. Comparison of coupled radiative flow solutions with Project Fire II flight data

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1. Effect of Thermal Ablation at the Fluid-Solid Interface of a Hypersonic Reentry Vehicle in Rarefied Flow Regime;International Journal of Computational Fluid Dynamics;2021-12-29

2. Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition;International Journal of Aeronautical and Space Sciences;2019-09-26

3. Aerodynamic Data of Non-Winged Re-entry Vehicles (RV-NW) - Capsules and Probes -;Aerodynamic Data of Space Vehicles;2014

4. Hypersonic Non-equilibrium Computations for Ionizing Air;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05

5. Predictions of Ablating Hypersonic Vehicles Using an Iterative Coupled Fluid/Thermal Approach;Journal of Thermophysics and Heat Transfer;2001-04

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