Author: Daniel GaffiePublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical Investigation of Supersonic Reacting Hydrogen Jets in a Hot Air Co-flow
Author: Daniel GaffiePublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical Investigation of the Supersonic Flow Through a SCRAMjet Including Hydrogen Injection and Combustion
Author: Leo Patrick O'HarePublisher:
ISBN:
Category :
Languages : en
Pages : 206
Book Description
Experimental and Numerical Investigation of Hydrogen Combustion in a Supersonic Flow
Author: Corin SegalPublisher:
ISBN:
Category : Combustion engineering
Languages : en
Pages : 324
Book Description
Numerical Study on Mixing and Combustion of Injecting Hydrogen Jet in a Supersonic Air Flow
Author: Masahiro TakahashiPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Composition Distribution and Equivalent Body Shape for a Reacting, Coaxial, Supersonic Hydrogen-air Flow
Author: Griffin Y. AndersonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 52
Book Description
Numerical Investigation of Hydrogen Strut Injections Into Supersonic Air Flows
Author: P. GerlingerPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Numerical Investigation of the Supersonic Flow Over a Rearward Facing Step with Transverse Hydrogen Injection
Author: Steven Mark SahmPublisher:
ISBN:
Category :
Languages : en
Pages : 254
Book Description
Studies of Hydrogen-air Supersonic Combustion at Low Densities
Author: James E. DrewryPublisher:
ISBN:
Category :
Languages : en
Pages : 35
Book Description
An investigation of supersonic combustion as related to propulsive systems for high Mach number, high altitude flight is described. A method of laboratory simulation is employed which is considered to be suitable for fundamental studies of diffusional-controlled supersonic combustion under conditions approaching those of actual flight. A numerical analysis of the mixing and chemical reaction processes in a hydrogen-air ducted flow system was carried out, using a computer code based upon boundary layer concepts and including the effects of finite-rate chemistry. Results of the numerical calculations have indicated the inlet conditions at which auto-ignition is expected to occur within a reasonable combustor length. Based on the numerical data obtained, a constant area-divergent area combustion chamber was designed and fabricated for the performance of experimental tests under conditions closely matching those of the numerical study. (Author).
Theoretical and Experimental Investigation of Supersonic Combustion
Author: Antonio FerriPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 136
Book Description
A theoretical and experimental investigation of mixing and supersonic combustion is presented. A review of the problem under investigation is given. Then an analysis of inviscid flow fields with a finite rate chemistry for a hydrogen-air reaction is presented, an an analysis of a turbulent mixing for flows with large density gradients with no chemical reaction is presented. The analysis is compared wit the experimental results. Results of the experiments in upersonic combustion are presented. (Author).
Numerical Investigation of the Supersonic Flow Over a Rearward Facing Step with Transverse Hydrogen Injection
Author: Harry Allen BermanPublisher:
ISBN:
Category :
Languages : en
Pages : 180
Book Description
