Oblique detonation stabilized on a hypervelocity projectile

Symposium (International) on Combustion

Volumn 26, Issue 2, 1996, Pages 3015-3022

  Kaneshige, Michael J ^a   Shepherd, J E ^a  

^a CALIFORNIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMBUSTION; HYDROGEN; MIXTURES; NITROGEN; OXYGEN; PRESSURE EFFECTS; PROJECTILES; SHOCK WAVES; STABILITY; SUPERSONIC FLOW; VELOCITY;

CRITICAL DAMKOHLER NUMBER; DETONATION WAVES; FLOW QUENCHING EFFECTS; HYPERVELOCITY PROJECTILE; OBLIQUE DETONATION;

DETONATION;

EID: 0030362569     PISSN: 00820784     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0082-0784(96)80145-7     Document Type: Article

References (21)

1. A missile technique for the study of detonation waves.
2. Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders
3. Dynamic Parameters of Gaseous Detonations