A swept fin-induced flow field with different height mounting gaps-Reference-Cited by-同舟云学术

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A swept fin-induced flow field with different height mounting gaps

Published:2021-01 Issue:1 Volume:34 Page:148-162
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

ZHANG Feng,YI Shihe,XU Xiwang^ORCID,NIU Haibo^ORCID,LU Xiaoge

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference44 articles.

1. X-43A Hypersonic vehicle technology development;Voland;Acta Astronaut,2006

2. Numerical investigation of flow in blunt-fin gap of hypersonic vehicles;Huang;Adv Aeronaut Sci Eng,2019

3. Shock wave-boundary-layer interactions;Babinsky,2011

4. Experimental study on fine thermal measurement of high speed aircraft wing rudder gap in shock wave tunnel;Wu;Acta Aerodyn Sin,2019

5. Review of the physics of swept-shock boundary layer interactions;Panaras;Prg Aerosp Sci,1996

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2. Experimental Investigation of the Hypersonic Boundary-Layer Transition Induced by the Wall-Mounted Cylinder;Journal of Thermophysics and Heat Transfer;2023-10

3. Experimental study on the hypersonic boundary layer transition induced by tandem cylinders;Experimental Thermal and Fluid Science;2023-07

4. Numerical study of discrete film cooling near the rudder shaft of a hypersonic air fin model;Numerical Heat Transfer, Part A: Applications;2023-04-03

5. Experimental investigation of expansion effect on shock wave boundary layer interaction near a compression ramp;Chinese Journal of Aeronautics;2022-12

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