The possibility of normal shock waves on a body with convex surfaces in inviscid transonic flow

1960 ◽  
Vol 11 (1) ◽  
pp. 51-58 ◽  
Author(s):  
George E. Gadd
Keyword(s):  
Shock Waves ◽  
Transonic Flow ◽  
Normal Shock ◽  
Convex Surfaces

Perturbation Procedures for Nonlinear Viscous Flows

1983 ◽  
Vol 50 (2) ◽  
pp. 265-269
Author(s):  
D. Nixon
Keyword(s):  
Perturbation Theory ◽  
Shock Waves ◽  
Transonic Flow ◽  
Stokes Equations ◽  
Viscous Flows ◽  
Two Dimensions ◽  
Experimental Results ◽  
Navier Stokes ◽  
Navier Stokes Equations

The perturbation theory for transonic flow is further developed for solutions of the Navier-Stokes equations in two dimensions or for experimental results. The strained coordinate technique is used to treat changes in location of any shock waves or large gradients.

Analysis of Normal Combustion Waves in CH4-Air System

2014 ◽  
Vol 656 ◽  
pp. 101-109 ◽  
Author(s):  
Daniel Eugeniu Crunteanu ◽  
Dan Racoti ◽  
Corneliu Berbente
Keyword(s):  
Shock Waves ◽  
Algebraic Equation ◽  
Combustion Wave ◽  
Normal Shock ◽  
Combustion Waves ◽  
Conservation Equations ◽  
One Dimensional ◽  
Air System ◽  
The One

In this study one analyses the detonation and deflagration waves starting with Euler one-dimensional conservative equations. We present two methods of computing the normal combustion waves and normal shock waves parameters. The second one, called Cpm method, uses the one dimensional conservation equations system of mass, impulse and energy reduced to an quadratic algebraic equation. Combustion wave ,in CH4-air system is presented as an application.

Stability of normal shock waves in diffusers

AIAA Journal ◽  
1987 ◽  
Vol 25 (11) ◽  
pp. 1515-1517 ◽  
Author(s):  
Kazuyasu Matsuo ◽  
Minoru Yaga ◽  
Hiroaki Mochizuki
Keyword(s):  
Shock Waves ◽  
Normal Shock
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