Numerical study of the cone angle effects on transition and convection heat transfer for hypersonic inflatable aerodynamic decelerator aeroshell-Reference-Cited by-同舟云学术

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Numerical study of the cone angle effects on transition and convection heat transfer for hypersonic inflatable aerodynamic decelerator aeroshell

Published:2020-01 Issue: Volume:110 Page:104406
ISSN:0735-1933
Container-title:International Communications in Heat and Mass Transfer
language:en
Short-container-title:International Communications in Heat and Mass Transfer

Author:

Zhao Yatian,Liu Hongkang,Liu Zaijie,Yan Chao

Funder

Academic Excellence Foundation of BUAA for PhD Students

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics

Reference41 articles.

1. Hughes, thermal analysis and testing of candidate materials for PAIDAE inflatable aeroshell;Del Corso,2011

2. Postflight analysis of inflatable reentry and descent technology blackout during earth reentry;Reynier;J. Spacecr. Rocket.,2009

3. Suborbital reentry demonstration of inflatable flare-type thin-membrane Aeroshell using a sounding rocket;Yamada;J. Spacecr. Rocket.,2015

4. Aerodynamic heating of inflatable aeroshell in orbital reentry;Takahashi;Acta Astronautica,2018

5. Aerothermodynamic analysis for deformed membrane of inflatable aeroshell in orbital reentry mission;Takahashi;Aerosp. Sci. Technol.,2019

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1. A production term study of delayed detached eddy simulation for turbulent near wake based on proper orthogonal decomposition;Physics of Fluids;2023-10-01

2. Heat Balance Features of Decelerator System Considering Real-Time Reliability;International Journal of Heat and Technology;2023-02-28

3. Assessment and improvement of k-ω-γ model for separation-induced transition prediction;Chinese Journal of Aeronautics;2022-11

4. A three-equation transition model with mechanical considerations;Chinese Journal of Aeronautics;2022-11

5. Application of improved k-ω-γ model to deformed hypersonic Inflatable Aerodynamic Decelerator aeroshell;Applied Thermal Engineering;2022-09

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