Numerical study on supersonic combustion with cavity-based fuel injection

DOI10.1016/J.IJHEATMASSTRANSFER.2003.07.004zbMath1083.76065OpenAlexW2154025038MaRDI QIDQ1434579

Cho Young Han, Seung Wook Baek, Kyung Moo Kim

Publication date: 12 July 2004

Published in: International Journal of Heat and Mass Transfer (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijheatmasstransfer.2003.07.004

zbMATH Keywords

total pressure losssupersonic air flow

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Combustion (80A25) Chemically reacting flows (80A32) Reaction effects in flows (76V05)

Related Items (5)

Drag force investigation of cavities with different geometric configurations in supersonic flow ⋮ Inverse estimation of inlet parameters in an axisymmetric cylindrical combustor with thermal radiation effect ⋮ Heat transfer -- a review of 2004 literature ⋮ MODELING OF SUPERSONIC COMBUSTION USING POINT IMPLICIT FINITE VOLUME METHOD ⋮ Inverse estimation of inlet parameters in diffusion-controlled turbulent combustion in an axisymmetric combustor

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