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Loiter performance of turbojet-powered aircraft performance determined by off-design cycle analysisLoitering performance of airplanes equipped with various turbojet engines was analytically investigated. The engines used in this analysis were selected to show the effects of various engine design variables. Engine performance was determined by means of an off-design cycle analysismaking use of experimentally determined component characteristics. The method of off-design cycle analysis is presented herein and is verified by a check with experimental data.
Document ID
19930094392
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Koutz, Stanley L
Date Acquired
August 16, 2013
Publication Date
February 1, 1952
Report/Patent Number
NACA-RM-E5129a
Report Number: NACA-RM-E5129a
Accession Number
93R23311
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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