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Static calibration of an ejector unit for simulation of jet engines in small-scale wind-tunnel modelsStatic calibration of ejector unit for simulation of jet engines in small-scale wind tunnel models of VTOL aircraft
Document ID
19670009622
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Gentry, G. L. (NASA Langley Research Center Hampton, VA, United States)
Margason, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TN-D-3867
Report Number: NASA-TN-D-3867
Accession Number
67N18951
Funding Number(s)
CONTRACT_GRANT: 721-01-00-18-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
EJECTOR
VTOL AIRCRAFT
JET ENGINE
WIND TUNNEL MODEL

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