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Equations and procedures for numerically calculating the aerodynamic characteristics of lifting rotorsEquations and procedures are presented for numerically determining the aerodynamic characteristics of lifting rotors. The equations are general and can account for stall and compressibility effects, as well as variations in hub and blade configurations, that are normally omitted from conventional analytical rotor treatments. The application of the method to solution by automatic computing machines is discussed.
Document ID
19930084602
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Gessow, Alfred
Date Acquired
August 16, 2013
Publication Date
October 1, 1956
Report/Patent Number
NACA-TN-3747
Accession Number
93R13892
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LOADS - ROTATING WINGS
WINGS, ROTATING - THEORY
AUTOGIROS
VIBRATION AND FLUTTER - ROTATING-WING AIRCRAFT
HELICOPTERS
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