Experimental and numerical study on the local unstart mechanism of hypersonic inlet-Reference-Cited by-同舟云学术

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Experimental and numerical study on the local unstart mechanism of hypersonic inlet

Published:2019-07 Issue: Volume:160 Page:216-221
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Liu Junbing,Fan Xiaoqiang,Tao Yuan,Liu Weidong

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference48 articles.

1. Starting Characteristics of Supersonic Inlets,AIAA Paper 1996-2914;Van Wie,1996

2. Planetary Flight Surge Faces Budget Realities;Dornheim,1990

3. Adaptive Unstructured Euler Simulations of Hypersonic Inlet Flow Starting, AIAA Paper 2001-1896;Timofeev,2001

4. Two-Dimensional Generic Inlet Unstart Detection at Mach 2.5-5.0, AIAA Paper 1995-6019;Hawkins,1995

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

2. Start/unstart hysteresis characteristics driven by embedded rocket of a rocket-based combined-cycle inlet;Physics of Fluids;2024-08-01

3. Experimental research on the flow mechanism of dual-separation unstart phenomenon in hypersonic inlet;Aerospace Science and Technology;2024-07

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