Numerical simulation of opposing sonic jets-Reference-Cited by-同舟云学术

Numerical simulation of opposing sonic jets

Published:1992-04 Issue:2 Volume:21 Page:229-233
ISSN:0045-7930
Container-title:Computers & Fluids
language:en
Short-container-title:Computers & Fluids

Author:

Nomura H.,Aso S.,Nishida M.

Publisher

Elsevier BV

Subject

General Engineering,General Computer Science

Reference16 articles.

1. Exploratory investigation of the effect of forward-facing jet on the bow shock of a blunt body in a Mach number of 6 free stream;Romeo;NASA TN D-1605,1963

2. An experimental investigation of a two-layer inviscid shock cap due to blunt-body injection;Baron;J. Fluid Mech.,1963

3. Contours for stagnation-point mass injection in hypersonic flow;Wang;AIAA Jl,1964

4. Flow field for sonic jet exhausting counter to a hypersonic main stream;Romeo;AIAA Jl,1965

5. An experimental investigation of stagnation point injection;Barbar;J. Spacecraft,1965

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