Simulation of shock-induced combustion past blunt projectiles using shock-fitting technique

Journal of Propulsion and Power

Volumn 12, Issue 3, 1996, Pages 518-526

  Ahuja, J K ^a,d   Kumar, A ^b,d,e   Singh, D J ^c,f   Tiwari, S N ^a,d  

^a OLD DOMINION UNIVERSITY   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c ANALYTICAL SERVICES AND MATERIALS INC   (United States)

^d Department of Mechanical Engineering ^*

^e Gas Dynamics Division

^f Analytical Section

Author keywords

[No Author keywords available]

Indexed keywords

AIR; BOUNDARY CONDITIONS; COMPUTATIONAL METHODS; FINITE DIFFERENCE METHOD; FLOW INTERACTIONS; HYDROGEN; MIXTURES; NAVIER STOKES EQUATIONS; PHYSICS; PROJECTILES; SHOCK WAVES; VISCOUS FLOW;

BLUNT PROJECTILES; MACH NUMBER; RANKINE HUGONIOT CONDITIONS; SHOCK COMBUSTION; SHOCK FITTING TECHNIQUE;

COMBUSTION;

EID: 0030145468     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/3.24065     Document Type: Article

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