Flow-Based Prediction for Self-Starting Limit of Two-Dimensional Hypersonic Inlets-Reference-Cited by-同舟云学术

Flow-Based Prediction for Self-Starting Limit of Two-Dimensional Hypersonic Inlets

Published:2016-03 Issue:2 Volume:32 Page:463-471
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Xie Wen-zhong,Ma Guang-fu,Guo Rong-wei,Chen Hao,Wen Yu-fen,Guo Shengmin¹

Affiliation:

1. Louisiana State University, Baton Rouge, Louisiana 70803

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35703

Reference28 articles.

1. HenryJ. R.AndrewsE. H.PinckneyS. Z.Jr.McClintonC. R. “Boundary Layer and Starting Problems on a Short Axisymmetric Scramjet Inlet,” NASA SP-216, 1969.

2. Starting criterion for hypersonic inlets

3. GoldbergT. J.HefnerJ. N. “Starting Phenomena for Hypersonic Inlets with Thick Boundary Layers at Mach 6,” NASA TN-D6280, 1971.

4. KantrowitzA.DonaldsonC. “Preliminary Investigation of Supersonic Diffuser,” NACA WRL-713, 1945.

5. Starting characteristics of supersonic inlets

Cited by 18 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. Prediction model for self-starting of hypersonic inlets with soft critical unstart mode;Physics of Fluids;2024-09-01

2. Scramjet Intake Aerodynamic Studies Using Sharp Interface Immersed Boundary Method;Defence Science Journal;2024-03-26

3. Generalized prediction for self-starting performance of two-dimensional hypersonic inlets;Physics of Fluids;2024-01-01