Numerical Analysis of RCS Jet in Hypersonic Flights

912063

09/01/1991

Event
International Pacific Air & Space Technolgy Conference
Authors Abstract
Content
A transversely injected jet into a hypersonic flow is simulated numerically in order to study the flow field of the injection jet in the hypersonic atmosphere, its heat flux on the body surface and the moments working on the body. The flowfields is governed by the two-dimentional Reynolds averaged full Navier-Stokes equations with an algebraic eddy viscosity model developed by Baldwin-Lomax. The governing equations are solved using the Harten-Yee type TVD and central difference schemes to the convex and viscous terms, respectively. The real gas effect is considered in the numerical analysis. The jets injected across the main flows of Mach 10 and 15 are compared.
Meta TagsDetails
DOI
https://doi.org/10.4271/912063
Pages
8
Citation
Inoue, Y., Hayashi, A., Fujiwara, T., Miyake, S. et al., "Numerical Analysis of RCS Jet in Hypersonic Flights," SAE Technical Paper 912063, 1991, https://doi.org/10.4271/912063.
Additional Details
Publisher
Published
Sep 1, 1991
Product Code
912063
Content Type
Technical Paper
Language
English