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Computer code for estimating installed performance of aircraft gas turbine engines. Volume 1: Final reportA computerized method which utilizes the engine performance data is described. The method estimates the installed performance of aircraft gas turbine engines. This installation includes: engine weight and dimensions, inlet and nozzle internal performance and drag, inlet and nacelle weight, and nacelle drag.
Document ID
19800004788
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
D180-25481-1-VOL-1
NASA-CR-159691
Report Number: D180-25481-1-VOL-1
Report Number: NASA-CR-159691
Accession Number
80N13043
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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