Combustion of a turbulent supersonic nonisobaric hydrogen jet in an accompanying supersonic air flow

Journal Article · Wed Dec 31 23:00:00 EST 1986 · Combust., Explos. Shock Waves (Engl. Transl.); (United States)

DOI:https://doi.org/10.1007/BF00862880· OSTI ID:6249559

Baranovskii, S I; Nadvorskii, A S; Perminov, V A

The authors investigate an axisymmetric supersonic turbulent jet of hydrogen issuing into a cotravelling supersonic jet of air and undergoing combustion. They focus on the influence of heat liberation on the static pressure and combustion processes in the mixing layer as well as on the influence exerted on the mixing process by the laminar aspects and the density ratio of the two jets. The combustion and flow are modeled mathematically; flow diagrams and reaction kinetics are also included.

• OSTI ID: 6249559
• Journal Information: Combust., Explos. Shock Waves (Engl. Transl.); (United States), Journal Name: Combust., Explos. Shock Waves (Engl. Transl.); (United States) Vol. 22:4; ISSN CESWA
• Country of Publication: United States
• Language: English

Related Subjects

08 HYDROGEN
080800* -- Hydrogen-- Properties & Composition
AIR
BOUNDARY LAYERS
CHEMICAL REACTION KINETICS
CHEMICAL REACTIONS
COMBUSTION
COMBUSTION KINETICS
DENSITY
DIFFERENTIAL EQUATIONS
ELEMENTS
EQUATIONS
FLOW RATE
FLUID FLOW
FLUIDS
FUEL-AIR RATIO
GAS FLOW
GASES
HEAT FLOW
HYDROGEN
JETS
KINETICS
LAMINAR FLOW
LAYERS
MATHEMATICAL MODELS
MIXING
NAVIER-STOKES EQUATIONS
NONMETALS
NOZZLES
OXIDATION
PARTIAL DIFFERENTIAL EQUATIONS
PHYSICAL PROPERTIES
PRESSURE EFFECTS
REACTION KINETICS
SUPERSONIC FLOW
THERMOCHEMICAL PROCESSES
TURBULENCE
VISCOSITY