Numerical investigations on flow and heat transfer characteristics of a high-enthalpy double-cone in thermal and chemical non-equilibrium for hypersonic propulsion-Reference-Cited by-同舟云学术

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Numerical investigations on flow and heat transfer characteristics of a high-enthalpy double-cone in thermal and chemical non-equilibrium for hypersonic propulsion

Published:2024-06 Issue: Volume:155 Page:107522
ISSN:0735-1933
Container-title:International Communications in Heat and Mass Transfer
language:en
Short-container-title:International Communications in Heat and Mass Transfer

Author:

Dai Chunliang,Sun Bo,Zhao Dan,Zhou Shengbing,Zhou Changsheng,Man Yanjin

Publisher

Elsevier BV

Reference59 articles.

1. Effects of vibrational nonequilibrium on hypersonic shock-wave/laminar boundary-layer interactions;Hao;Int. Commun. Heat Mass Transf.,2018

2. Progress in shock wave/boundary layer interactions;Gaitonde;Prog. Aerosp. Sci.,2015

3. Hypersonic shock impingement on a heated flat plate at Mach 7 flight enthalpy;Chang;J. Fluid Mech.,2021

4. Proper orthogonal and dynamic mode decomposition analyses of nonlinear combustion instabilities in a solid-fuel ramjet combustor;Li;Therm. Sci. Eng. Prog.,2022

5. The implications of dual cavity location in a strut-mounted scramjet combustor;Rajesh;Int. Commun. Heat Mass Transf.,2023

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