Investigation on transonic round convex-corner flows-Reference-Cited by-同舟云学术

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Investigation on transonic round convex-corner flows

Published:2014-08 Issue: Volume:37 Page:20-25
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Chung Kung-Ming^ORCID,Chang Po-Hsiung^ORCID,Chang Keh-Chin,Lu Frank K.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference24 articles.

1. The wall pressure signature of transonic shock/boundary layer interaction;Bernardini;J. Fluid Mech.,2010

2. A. Bolonkin, G.B. Gilyard, Estimated benefits of variable-geometry wing camber control for transport aircraft, NASA TM-1999-206586, Oct. 1999.

3. Transition of subsonic and transonic expansion-corner flows;Chung;J. Aircr.,2000

4. Investigation on transonic convex-corner flows;Chung;J. Aircr.,2002

5. Unsteadiness of transonic convex-corner flows;Chung;Exp. Fluids,2004

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Howling in a Model-Scale Nozzle Related to Shock-Induced Boundary-Layer Separation at the Nozzle Exit;AIAA AVIATION 2023 Forum;2023-06-08

2. An experimental study on transonic swept convex-corner flows;Aerospace Science and Technology;2019-01

3. Investigation of transonic bi-convex corner flows;Aerospace Science and Technology;2014-12

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