Author: David F. DyerPublisher:
ISBN:
Category : Combustion
Languages : en
Pages : 84
Book Description
Combustion of Hydrogen Injected Into a Supersonic Airstream
Author: David F. DyerPublisher:
ISBN:
Category : Combustion
Languages : en
Pages : 84
Book Description
Combustion of Hydrogen Injected Into a Supersonic Airstream (the SHIP Computer Program)
Author: N. C. MarkatosPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 132
Book Description
NASA Technical Note
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 938
Book Description
NASA Technical Paper
Author: Publisher:
ISBN:
Category : Science
Languages : en
Pages : 50
Book Description
NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 614
Book Description
Combustion of Hydrogen in a Two-dimensional Duct with Step Fuel Injectors
Author: James M. EggersPublisher:
ISBN:
Category : Combustion
Languages : en
Pages : 68
Book Description
An investigation of the combustion of hydrogen perpendicularly injected from step fuel injectors into a Mach 2.72, 2100 K vitiated test gas was conducted. The model simulated the flow between the center and side struts of an integrated scramjet module at Mach 7 flight and an altitude of 29 km. Parametric variation included equivalence ratio, fuel dynamic pressure ratio, and area distribution of the model. The overall area ratio of the model was held constant at 2.87. The data analysis indicated that no measurable improvement in mixing or combustion efficiency was obtained by varying the fuel dynamic pressure ratio from 0.79 to 2.45. Computations indicated approximately 80 percent of the fuel was mixed so that it could react; however, only approximately 50 percent of the mixed fuel actually reacted in two test configurations, and 74 percent in later tests where less area expansion of the flow occurred.
Criteria for Self-ignition of Supersonic Hydrogen-air Mixtures
Author: Paul W. HuberPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 64
Book Description
Criteria for Self-ignition of Supersonic Hydrogen-air Mixtures
Author: Paul William HuberPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 64
Book Description
Thermal Design and Analysis of a Hydrogen-burning Wind Tunnel Model of an Airframe-integrated Scramjet
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 88
Book Description
The Flow Field of an Underexpanded H2 Jet Coaxially Injected Into a Hot Free Or Ducted Supersonic Jet of Air Or Nitrogen
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
