The influence of the sinusoidal shock generator on the mixing rate of multi hydrogen jets at supersonic flow-Reference-Cited by-同舟云学术

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The influence of the sinusoidal shock generator on the mixing rate of multi hydrogen jets at supersonic flow

Published:2020-01 Issue: Volume:96 Page:105579
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Li Yicheng,Barzegar Gerdroodbary M.,Moradi R.,Babazadeh Houman

Funder

China Postdoctoral Science Foundation

National Natural Science Foundation of China

National Key Research and Development Program of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference59 articles.

1. Characteristics of dual transverse injection in scramjet combustor, part 1: mixing;Lee;J. Propuls. Power,2006

2. The influence of upstream wavy surface on the mixing zone of the transverse hydrogen jet at supersonic free stream;Barzegar Gerdroodbary;Aerosp. Sci. Technol.,2019

3. Molecular weight and injector configuration effects on the transverse injection flow field properties in supersonic flows;Huang;Aerosp. Sci. Technol.,2014

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

5. Molecular weight and injector configuration effects on the transverse injection flow field properties in supersonic flows;Huang;Aerosp. Sci. Technol.,2014

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