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Dynamic pressure and thrust characteristics of cold jets discharging from several exhaust nozzles designed for vtol downwash suppressionExhaust nozzle testing using cold air flow to find effect of exit design on thrust & jet wake dynamic pressure for use in vtol downwash suppression
Document ID
19640009044
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Higgins, C. C. (Boeing Co. Renton, WA, United States)
Wainwright, T. W. (Boeing Co. Renton, WA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1964
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-2263
Report Number: NASA-TN-D-2263
Accession Number
64N18958
Funding Number(s)
CONTRACT_GRANT: NASW-461
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DYNAMIC PRESSURE
VTOL AIRCRAFT
AIRFLOW
EXHAUST NOZZLE

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