Transient simulation of superdetonative mode initiation process in scram-accelerator

Symposium (International) on Combustion

Volumn 26, Issue 2, 1996, Pages 2957-2963

  Choi, Jeong Yeol ^a   Jeung, In Seuck ^a   Yoon, Youngbin ^a  

^a Department of Aerospace Engineering Seoul National University Seoul   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

AIR; COMPUTER SIMULATION; HYDROGEN; IGNITION; NAVIER STOKES EQUATIONS; PROJECTILES; PROPULSION; SHOCK WAVES; SUPERSONIC FLOW;

POINT IMPLICIT METHOD; RAM ACCELERATOR; SUPERDETONATIVE MODE; UPWIND BIASED THIRD ORDER SCHEME;

DETONATION;

EID: 0030354120     PISSN: 00820784     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0082-0784(96)80138-X     Document Type: Article

References (26)

1. Operational characteristics of the thermally choked ram accelerator
2. Magnetic detector for projectiles in tubes
3. Approximate solutions for oblique detonations in the hypersonic limit