Gradients at a curved shock in reacting flow

Shock Waves

Volumn 8, Issue 1, 1998, Pages 11-21

  Hornung, H G ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

Crocco point; Detonation; Mach reflection; Pressure deflection map; Shock stability; Sonic line; Streamline curvature; Vorticity

Indexed keywords

EID: 19444370174     PISSN: 09381287     EISSN: None     Source Type: Journal    
DOI: 10.1007/s001930050094     Document Type: Article

References (11)

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4. Hornung HG (1976) Non-equilibrium ideal-gas dissociation after a curved shock wave. J. Fluid Mech. 74:143
5. Hornung HG, Smith GH (1979) The influence of relaxation on shock detachment. J. Fluid Mech. 3:225
6. Kewley DJ, Hornung HG (1974) Non-equilibrium nitrogen flow over a wedge 64:725
7. Lighthill MJ (1949) The flow behind a stationary shock. Phil. Mag. 40:214
8. Mölder S (1971) Reflection of curved shock waves in steady supersonic flow. CASI Trans. 40:73-80
9. Mölder S (1972) Polar streamline directions at the triple point of Mach interaction of shock waves. CASI Trans. 5:88-89
10. Munk MM, Prim RC (1948) Surface-pressure gradient and shock-front curvature at the edge of a plane ogive with attached shock front. J. aeron. Sci. 15:691
11. Oswatitsch K (1952) Gasdynamik. Springer