Prediction of self-starting limit of two-dimensional supersonic inlets considering viscous effects-Reference-Cited by-同舟云学术

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Prediction of self-starting limit of two-dimensional supersonic inlets considering viscous effects

Published:2020-11 Issue: Volume:106 Page:106229
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Xie Wen-Zhong,Yang Wei,Jin Yi,Yang Shuzi,Zeng Cheng,Guo Shengmin^ORCID

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference21 articles.

1. Scramjet Propulsion, Progress in Astronautics and Aeronautics,2000

2. Preliminary investigation of supersonic diffusers;Kantrowitz,1945

3. Limiting contractions for starting simple ramp-type scramjet intakes with overboard spillage;Veillard;J. Propuls. Power,2008

4. Starting characteristics of Prandtl–Meyer scramjet intakes with overboard spillage;Moradian;J. Propuls. Power,2018

5. Shock Wave–Boundary-Layer Interactions;Babinsky,2011

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