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Experimental aerodynamic and acoustic model testing of the Variable Cycle Engine (VCE) testbed coannular exhaust nozzle system: Comprehensive data reportThe component detail design drawings of the one sixth scale model of the variable cycle engine testbed demonstrator exhaust syatem tested are presented. Also provided are the basic acoustic and aerodynamic data acquired during the experimental model tests. The model drawings, an index to the acoustic data, an index to the aerodynamic data, tabulated and graphical acoustic data, and the tabulated aerodynamic data and graphs are discussed.
Document ID
19800017802
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Nelson, D. P.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Morris, P. M.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
PWA-5550-40
NASA-CR-159711
Report Number: PWA-5550-40
Report Number: NASA-CR-159711
Accession Number
80N26301
Funding Number(s)
CONTRACT_GRANT: NAS3-20061
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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