Tomography-like flow visualization of a hypersonic inward-turning inlet-Reference-Cited by-同舟云学术

Tomography-like flow visualization of a hypersonic inward-turning inlet

Published:2021-01 Issue:1 Volume:34 Page:44-49
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

LI Yiming^ORCID,LI Zhufei,YANG Jiming

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference25 articles.

1. You YC. An overview of the advantages and concerns of hypersonic inward turning inlets. Reston: AIAA; 2011. Report No.: AIAA-2011-2269.

2. Bulman M, Siebenhaar A. The rebirth of round hypersonic propulsion. Reston,: AIAA; 2006. Report No: AIAA-2006-5035.

3. Bisek NJ. High-fidelity simulations of the HIFiRE-6 flow path at angle of attack. Reston: AIAA; 2016. Report No.: AIAA-2016-4276.

4. Wang WX, Zhu T, Zhang RT, et al. Flow field reconstruction of hypersonic inward turning inlet based on configuration. Acta Aeronaut et Astronaut Sin 2020; 41(3): 123493[Chinese].

5. Design method with controllable velocity direction at throat for inward-turning inlets;QIAO;Chin J Aeronaut,2019

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