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Computer code for estimating installed performance of aircraft gas turbine engines. Volume 3: Library of mapsA computerized method which utilizes the engine performance data and estimates the installed performance of aircraft gas turbine engines is presented. This installation includes: engine weight and dimensions, inlet and nozzle internal performance and drag, inlet and nacelle weight, and nacelle drag. The use of two data base files to represent the engine and the inlet/nozzle/aftbody performance characteristics is discussed. The existing library of performance characteristics for inlets and nozzle/aftbodies and an example of the 1000 series of engine data tables is presented.
Document ID
19800004790
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kowalski, E. J. (Boeing Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
D180-25481-3-VOL-3
NASA-CR-159693
Accession Number
80N13045
Funding Number(s)
CONTRACT_GRANT: NAS3-21238
PROJECT: RTOP 505-05-52
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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