Numerical Simulation of 2-D Full-scale Flow Field for Hypersonic Vehicle

LEI  Hongshuai; WANG  Zhenqing; FU  Ji; LV  Hongqing

doi:10.15892/j.cnki.djzdxb.2012.03.027

Journal of Projectiles, Rockets, Missiles and Guidance >

2012 , Vol. 32 >Issue 3: 157 - 160

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2012.03.027

BALLISIIC AND AIRDYNAMICS

Numerical Simulation of 2-D Full-scale Flow Field for Hypersonic Vehicle

LEI Hongshuai ,
WANG Zhenqing ,
FU Ji ,
LV Hongqing

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College of Aerospace and Civil Engineering, Harbin Engineering University, Harbin 150001, China

Received date: 2011-07-21

Online published: 2025-05-29

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Abstract

In this paper, the 2-D ful-scale flow field, in different mach number and attack angel, was analyz while considered the hydrogen/ air reaction based on the finite volume method and Roe' form. Simulation results show that the engine perform well when using the optimized geometric parameter (8°/6°/7°) in design situation, there were enough pressure and mass of air to make the engine be in best condition.

Key words： hypersonic vehicle; full-scale flow field; chemical reaction; numerical simulation

Cite this article

LEI Hongshuai , WANG Zhenqing , FU Ji , LV Hongqing . Numerical Simulation of 2-D Full-scale Flow Field for Hypersonic Vehicle[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2012 , 32(3) : 157 -160 . DOI: 10.15892/j.cnki.djzdxb.2012.03.027

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