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Exhaust jet wake and thrust characteristics of several nozzles designed for VTOL DOWNWASH suppression. Tests in and out of ground effect with 70 deg F and 1200 deg F nozzle discharge temperaturesJet wake degradation and thrust characteristics of exhaust nozzles designed for VTOL downwash suppression and fuselage and ground effects
Document ID
19660006071
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Higgins, C. C. (Boeing Co. Renton, WA, United States)
Kelly, D. P. (Boeing Co. Renton, WA, United States)
Wainwright, T. W. (Boeing Co. Renton, WA, United States)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-373
Report Number: NASA-CR-373
Accession Number
66N15360
Funding Number(s)
CONTRACT_GRANT: NASW-908
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
EXHAUST NOZZLE
DOWNWASH
JET NOZZLE
WAKE
JET THRUST

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