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F100 exhaust nozzle area controlThe details of the F100 nozzle mechanism design are highlighted, placing particular emphasis upon the evolution of design constraints or drivers from initial concept through current operational deployment. A kinematic description of the area control mechanism is given, and several environmental constraints which complicate the normal mechanism design process are discussed.
Document ID
19800015022
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kozlin, J. R. (Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
August 10, 2013
Publication Date
May 1, 1980
Publication Information
Publication: NASA. Langley Res. Center Proc. of the 14th Aerospace Mech. Symp.
Subject Category
Aircraft Propulsion And Power
Accession Number
80N23513
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19800015004Collected WorksProceedings of the 14th Aerospace Mechanisms Symposium19800015004Collected WorksProceedings of the 14th Aerospace Mechanisms Symposium
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