Three-dimensional structure of stabilization of oblique detonation wave in hypersonic flow-Reference-Cited by-同舟云学术

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Three-dimensional structure of stabilization of oblique detonation wave in hypersonic flow

Published:1998-01 Issue:2 Volume:27 Page:2207-2214
ISSN:0082-0784
Container-title:Symposium (International) on Combustion
language:en
Short-container-title:Symposium (International) on Combustion

Author:

Viguier C.,Gourara A.,Desbordes D.

Publisher

Elsevier BV

Reference31 articles.

1. Ram accelerator - A new chemical method for accelerating projectilesto ultrahigh velocities

2. Morphology of standing oblique detonation waves

3. Detonation structures behind oblique shocks

4. Proceedings of 3rd Asian-Pacific Symposium on Combustion and Energy Utilisation;Figueira Da Silva,1995

5. Twenty-Sixth Symposium (International) on Combustion;Viguier,1996

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1. Numerical study on the internal/external flow and thrust-drag characteristics of oblique detonation engine-based aircraft;Aerospace Science and Technology;2024-09

2. High-fidelity Simulation of Oblique Detonation Waves;AIAA SCITECH 2024 Forum;2024-01-04

3. Formation and Evolution of Cellular Structures in Wedge-Induced Oblique Detonations;International Journal of Aerospace Engineering;2023-03-29

4. Oblique Detonation Wave Control with O3 and H2O2 Sensitization in Hypersonic Flow;Energies;2022-06-04

5. Numerical investigation on movement of triple points on oblique detonation surfaces;Physics of Fluids;2022-06

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