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Effect of rotor-blade twist and plan-form taper on helicopter hovering performance
Document ID
19930082219
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gessow, Alfred
Date Acquired
August 16, 2013
Publication Date
February 1, 1948
Report/Patent Number
NACA-TN-1542
Accession Number
93R11509
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROTOR BLADES - TWIST
EQUATIONS - HELICOPTERS
HELICOPTERS - PERFORMANCE CALCULATIONS
CHARTS - HELICOPTERS
PROPELLERS, HELICOPTER

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