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NASA Lewis F100 engine testingTwo builds of an F100 engine model derivative (EMD) engine were evaluated for improvements in engine components and digital electronic engine control (DEEC) logic. Two DEEC flight logics were verified throughout the flight envelope in support of flight clearance for the F100 engine model derivative program (EMPD). A nozzle instability and a faster augmentor transient capability was investigated in support of the F-15 DEEC flight program. Off schedule coupled system mode fan flutter, DEEC nose-boom pressure correlation, DEEC station six pressure comparison, and a new fan inlet variable vane (CIVV) schedule are identified.
Document ID
19860015875
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Werner, R. A. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Willoh, R. G., Jr. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Abdelwahab, M. (NASA Hugh L. Dryden Flight Research Center Edwards, CA, United States)
Date Acquired
August 12, 2013
Publication Date
March 1, 1984
Publication Information
Publication: Digital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PAPER-4
Report Number: PAPER-4
Accession Number
86N25346
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19860015871Collected WorksDigital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane19860015871Collected WorksDigital Electronic Engine Control (DEEC) Flight Evaluation in an F-15 Airplane
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