Numerical simulation of inviscid flows with hydrogen combustion behind shock waves and in detonation waves
Journal Article
·
· Combustion, Explosion and Shock Waves
A new numerical algorithm for simulation of nonequilibrium chemically reacting flows of an inviscid multicomponent gas is described. Application of this algorithm to the numerical solution of several problems of air-hydrogen mixture combustion in oblique detonation waves is demonstrated.
- Sponsoring Organization:
- USDOE
- OSTI ID:
- 229683
- Journal Information:
- Combustion, Explosion and Shock Waves, Vol. 31, Issue 3; Other Information: PBD: Nov 1995; TN: Translated from Fizika Goreniya i Vzryva; 31: No. 3, 118-133(May-Jun 1995)
- Country of Publication:
- United States
- Language:
- English
Similar Records
H{sub 2}-air and CH{sub 4}-air detonations and combustions behind oblique shock waves
Mass exchange and combustion in a laminar boundary layer behind a shock wave when a detonation is propagated in unmixed two-phase systems
Mass exchange and combustion in a laminar boundary layer behind a shock wave when a detonation is propagated in unmixed two-phase systems
Book
·
Sat Dec 31 00:00:00 EST 1994
·
OSTI ID:229683
Mass exchange and combustion in a laminar boundary layer behind a shock wave when a detonation is propagated in unmixed two-phase systems
Journal Article
·
Fri Jul 01 00:00:00 EDT 1983
· Combust., Explos. Shock Waves (Engl. Transl.); (United States)
·
OSTI ID:229683
Mass exchange and combustion in a laminar boundary layer behind a shock wave when a detonation is propagated in unmixed two-phase systems
Journal Article
·
Fri Jul 01 00:00:00 EDT 1983
· Combust., Explos. Shock Waves (Engl. Transl.); (United States)
·
OSTI ID:229683