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Computer program for design-point performance of turbojet and turbofan engine cyclesFortran 7094 computer program for calculation of design point performance of turbojet and turbofan engine cycles, and thermodynamic equations
Document ID
19670009070
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Vanco, M. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1967
Subject Category
Computers
Report/Patent Number
NASA-TM-X-1340
Report Number: NASA-TM-X-1340
Accession Number
67N18399
Funding Number(s)
CONTRACT_GRANT: 720-03-01-35-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THERMODYNAMICS
PERFORMANCE CHARACTERISTICS
TURBOJET ENGINE
TURBOFAN ENGINE
COMPUTER PROGRAM

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