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The jet engine design that can drastically reduce oxides of nitrogenThe problem is analyzed for the case of hydrogen fuel, taking into account supersonic and hypersonic vehicles using scramjet engines. The combustion in scramjets occurs at very high velocity and in a short time. In scramjet combustor designs, two different criteria can be used to design the engine. The amount of NO formed in the diffusion flame depends substantially on the maximum temperature reached. Effects of changing the mode of combustion from a diffusion flame to a heat conduction flame are considered, giving attention to the amount of NO produced in an engine of a given design.
Document ID
19740036047
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ferri, A.
Agnone, A.
(New York University Bronx, N.Y., United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 74-160
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Washington, DC
Start Date: January 30, 1974
End Date: February 1, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A18797
Funding Number(s)
CONTRACT_GRANT: NGR-33-016-131
Distribution Limits
Public
Copyright
Other

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