Author: N. C. Markatos
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 130
Book Description
Combustion of hydrogen injected into a supersonic airstream (the ship computer program)
Author: N. C. Markatos
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 130
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 130
Book Description
Combustion of Hydrogen Injected Into a Supersonic Airstream
Author: David F. Dyer
Publisher:
ISBN:
Category : Combustion research
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Combustion research
Languages : en
Pages : 84
Book Description
Combustion of Hydrogen Injected Into a Supersonic Airstream (the SHIP Computer Program)
Author: N. C. Markatos
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 132
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 132
Book Description
Supersonic Combustion of Hydrogen Injected Perpendicular to a Ducted Vitiated Airstream
A Study of the Mixing of Hydrogen Injected Normal to a Supersonic Airstream
Author: R. Clayton Rogers
Publisher:
ISBN:
Category : Hydrogen as fuel
Languages : en
Pages : 60
Book Description
Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected normal to supersonic airstreams.
Publisher:
ISBN:
Category : Hydrogen as fuel
Languages : en
Pages : 60
Book Description
Jet to free-stream dynamic pressure ratio effects on penetration and mixing of hydrogen injected normal to supersonic airstreams.
Mixing and Combustion of Hydrogen in a Supersonic Airstream
Author: Malcolm Thomas Jacques
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
The report is concerned with the mixing and combustion of hydrogen in a high enthalpy Mach 3.5 airstream, in which the conditions are such that the combustion process is mixing limited. The high enthalpy conditions are obtained using a combustion driven hypersonic shock tunnel. A gas composition probe having a response time of 0.25 msec. has been constructed and used in contamination and combustion studies. Combustion results have been obtained from a 2-D Mach 3.5 test section using both a mid-stream vortex generating injector and a plain wedge injector. The turbulent mixing characteristics of the two wakes were determined using a semi-quantitative approach which utilizes well established relationships of structural turbulence theory. The results of this analysis showed the importance of the initial turbulence generation on the overall mixing process. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
The report is concerned with the mixing and combustion of hydrogen in a high enthalpy Mach 3.5 airstream, in which the conditions are such that the combustion process is mixing limited. The high enthalpy conditions are obtained using a combustion driven hypersonic shock tunnel. A gas composition probe having a response time of 0.25 msec. has been constructed and used in contamination and combustion studies. Combustion results have been obtained from a 2-D Mach 3.5 test section using both a mid-stream vortex generating injector and a plain wedge injector. The turbulent mixing characteristics of the two wakes were determined using a semi-quantitative approach which utilizes well established relationships of structural turbulence theory. The results of this analysis showed the importance of the initial turbulence generation on the overall mixing process. (Author).
Mixing and Combustion of Hydrogen in a Supersonic Airstream
Author: Malcolm Thomas Jacques
Publisher:
ISBN:
Category :
Languages : en
Pages : 190
Book Description
The report is concerned with the mixing and combustion of hydrogen in a high enthalpy Mach 3.5 airstream, in which the conditions are such that the combustion process is mixing limited. The high enthalpy conditions are obtained using a combustion driven hypersonic shock tunnel. A gas composition probe having a response time of 0.25 msec. has been constructed and used in contamination and combustion studies. Combustion results have been obtained from a 2-D Mach 3.5 test section using both a mid-stream vortex generating injector and a plain wedge injector. The turbulent mixing characteristics of the two wakes were determined using a semi-quantitative approach which utilizes well established relationships of structural turbulence theory. The results of this analysis showed the importance of the initial turbulence generation on the overall mixing process. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 190
Book Description
The report is concerned with the mixing and combustion of hydrogen in a high enthalpy Mach 3.5 airstream, in which the conditions are such that the combustion process is mixing limited. The high enthalpy conditions are obtained using a combustion driven hypersonic shock tunnel. A gas composition probe having a response time of 0.25 msec. has been constructed and used in contamination and combustion studies. Combustion results have been obtained from a 2-D Mach 3.5 test section using both a mid-stream vortex generating injector and a plain wedge injector. The turbulent mixing characteristics of the two wakes were determined using a semi-quantitative approach which utilizes well established relationships of structural turbulence theory. The results of this analysis showed the importance of the initial turbulence generation on the overall mixing process. (Author).
Mixing of Hydrogen Injected from Multiple Injectors Normal to a Supersonic Airstream
Author: R. Clayton Rogers
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 42
Book Description
Three Dimensional Computations of Transverse Hydrogen Jet Combustion in a Supersonic Airstream
A Study of the Combustion of Aluminum Borohydride in a Small Supersonic Wind Tunnel
Author: Harrison Allen
Publisher:
ISBN:
Category : Aluminum compounds
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aluminum compounds
Languages : en
Pages : 20
Book Description