AEROSPACE SHANGHAI, Volume. 42, Issue 2, 166(2025)
Numerical Study on the Oblique Detonation Wave Induced by a Transverse Hydrogen Jet
Fig. 1. Schematic diagram of an ODW engine and the corresponding jet/wedge-induced ODW computational domain
Fig. 3. Comparison of the numerical and literature results of the distributions of pressure and temperature along the wedge surface
Fig. 4. Comparison of the temperature contours of the ODW with and without a jet at different wedge angles
Fig. 5. Comparison of the temperature contours of the ODW initiation region with different grid sizes
Fig. 6. Comparison of the distributions of the temperature and H2 mass fraction with different grid sizes along y = 0.008 m
Fig. 7.
Fig. 8. Temperature contours of the jet-induced ODW at different jet dynamic pressure ratios
Fig. 9. ODW initiation lengths and ODW heights at the combustor exit under different jet dynamic pressure ratios
Fig. 10. Temperature contours of the jet-induced ODW at different jet angles
Fig. 11. ODW initiation lengths and ODW heights at the combustor exit at different jet angles
Fig. 12. Schematic diagram of the flow field morphology of the jet-induced ODW by different initiation types
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Junhan MA, Ruiyang YAO, Bin ZHANG. Numerical Study on the Oblique Detonation Wave Induced by a Transverse Hydrogen Jet[J]. AEROSPACE SHANGHAI, 2025, 42(2): 166
Category: Simulation and Analysis
Received: Sep. 30, 2024
Accepted: --
Published Online: May. 26, 2025
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