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Exploratory wind tunnel tests of the NASA- Bell recovery rotorExploratory wind tunnel tests of recovery rotor concept in axial flow
Document ID
19670008307
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Erb, L. H. (Bell Helicopter Co. Fort Worth, TX, United States)
Date Acquired
August 3, 2013
Publication Date
August 5, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-73065
REPT.-543-099-004
Report Number: NASA-CR-73065
Report Number: REPT.-543-099-004
Accession Number
67N17636
Funding Number(s)
CONTRACT_GRANT: NAS2-1165
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXIAL FLOW
WIND TUNNEL
ROTOR AERODYNAMICS
RECOVERY DEVICE

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