Shock layer instability near the Newtonian limit of hypervelocity flows

Physics of Fluids

Volumn 13, Issue 8, 2001, Pages 2394-2402

  Hornung, H G ^a   Lemieux, P ^b  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

^b EXPONENT INC   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CARBON DIOXIDE; HYPERSONIC FLOW; PROPANE; SHOCK WAVES;

SHEAR LAYERS;

NEWTONIAN FLOW;

COMPUTATIONAL MODEL; HYPERSONIC FLOW; VORTICITY;

EID: 0035424062     PISSN: 10706631     EISSN: None     Source Type: Journal    
DOI: 10.1063/1.1383591     Document Type: Article

References (11)

1. Dynamics of a dissociating gas
2. The effect of walls on a spatially growing supersonic shear layer
3. Laminar boundary layer stability experiments on a cone at Mach 8, Part 2: Blunt cone
4. On rotational flows
5. Amrita-A computational facility (for CFD modeling)
6. Detonation initiation by hypervelocity projectiles
7. Kinetic phase transition in molecular gases and its effect on flow formation behind a detached shock wave