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Operational procedure for computer program for design point characteristics of a gas generator or a turbojet lift engine for V/STOL applicationsThe computer program described calculates the design-point characteristics of a gas generator or a turbojet lift engine for V/STOL applications. The program computes the dimensions and mass, as well as the thermodynamic performance of the model engine and its components. The program was written in FORTRAN 4 language. Provision has been made so that the program accepts input values in either SI Units or U.S. Customary Units. Each engine design-point calculation requires less than 0.5 second of 7094 computer time.
Document ID
19730003067
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Krebs, R. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
E-6968
NASA-TM-X-2656
Report Number: E-6968
Report Number: NASA-TM-X-2656
Accession Number
73N11794
Funding Number(s)
PROJECT: RTOP 501-14
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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