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Direct-connect test of a hydrogen-fueled three-strut injector for an integrated modular scramjet engineThe study aims at illustrating the effects of strut and injector interactions and strut wakes not totally simulated in previous, less complex, direct-connect hardware. In addition, the influence of the relative location of the injectors on opposite sides of each strut and the effect of injector spacing are evaluated. It is shown that better mixing efficiency is attained by locating the fuel injectors on opposite sides of a strut so that the jets come together, rather than being staggered, in the strut wake. It is not possible to determine the combustion efficiency by means of a one-dimensional analysis of the wall pressure.
Document ID
19780030345
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mcclinton, C. R.
(NASA Langley Research Center Hampton, VA, United States)
Gooderum, P. B.
(NASA Langley Research Center High-Speed Aerodynamics Div., Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
August 1, 1977
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: Combustion Meeting
Location: Colorado Springs, CO
Start Date: August 15, 1977
End Date: August 17, 1977
Sponsors: Joint Army-Navy-NASA-Air Force Interagency Propulsion Committee
Accession Number
78A14254
Distribution Limits
Public
Copyright
Other

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