The influence of the wedge shock generator on the vortex structure within the trapezoidal cavity at supersonic flow-Reference-Cited by-同舟云学术

The influence of the wedge shock generator on the vortex structure within the trapezoidal cavity at supersonic flow

Published:2020-03 Issue: Volume:98 Page:105695
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Zhixiong,Manh Tran Dinh,Barzegar Gerdroodbary M.,Nam Nguyen Dang,Moradi R.,Babazadeh Houman

Funder

NSFC

Department of Science and Technology of Fujian Province

Fujian Province Natural Science Foundation

Australia ARC DECRA

Publisher

Elsevier BV

Subject

Aerospace Engineering

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3. The influence of the sinusoidal shock generator on the mixing rate of multi hydrogen jets at supersonic flow;Li;Aerosp. Sci. Technol.,2020

4. Effect of the injector configuration for opposing jet on the drag and heat reduction;Li;Aerosp. Sci. Technol.,2016

5. Detailed parametric investigations on drag and heat flux reduction induced by a combinational spike and opposing jet concept in hypersonic flows;Min;Int. J. Heat Mass Transf.,2018

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