Numerical investigation of supersonic flow over a parachute-like configuration including turbulent flow effects-Reference-Cited by-同舟云学术

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Numerical investigation of supersonic flow over a parachute-like configuration including turbulent flow effects

Published:2022-02 Issue: Volume:121 Page:107330
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Fan Jianhui,Hao Jiaao^ORCID,Wen Chih-Yung^ORCID,Xue Xiaopeng

Funder

National Natural Science Foundation of China

Natural Science Foundation of Hunan Province

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference50 articles.

1. Aerodynamic decelerators for planetary exploration: past, present, and future;Cruz,2006

2. Numerical investigation of the supersonic stabilizing parachute's heating loads;Qu;Aerosp. Sci. Technol.,2019

3. Review of unsteady aerodynamics of supersonic parachutes;Xue;Prog. Aerosp. Sci.,2021

4. The Tianwen-1 guidance, navigation, and control for Mars entry, descent, and landing;Huang;Space: Sci. Technol.,2021

5. Ballistic range testing data analysis of Tianwen-1 Mars entry capsule;Wei;Space: Sci. Technol.,2021

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