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ENGINEL: A single rotor turbojet engine cycle match performance programENGINEL is a computer program which was developed to generate the design and off-design performance of a single rotor turbojet engine with or without afterburning using a cycle match procedure. It is capable of producing engine performance over a wide range of altitudes and Mach numbers. The flexibility, of operating with a variable geometry turbine, for improved off-design fuel consumption or with a fixed geometry turbine as in conventional turbojets, has been incorporated. In addition, the option of generation engine performance with JP4, liquid hydrogen or methane as fuel is provided.
Document ID
19780004146
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lovell, W. A.
(Vought Corp. Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-145267
Report Number: NASA-CR-145267
Accession Number
78N12089
Funding Number(s)
CONTRACT_GRANT: NAS1-13500
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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