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Helicopter rotor noise generation.Distributive loading rotational theory for helicopter rotor noise generation, considering steady and fluctuating force radiation and impulsive blade slap
Document ID
19690057233
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leverton, J. W.
Wright, S. E.
Date Acquired
August 5, 2013
Publication Date
January 1, 1969
Publication Information
Publisher: CORNELL AERONAUTICAL LAB., INC.,
Subject Category
Aerodynamics
Meeting Information
Meeting: AERODYNAMICS OF ROTARY WING AND V/STOL AIRCRAFT, SYMPOSIUM
Location: BUFFALO, NY
Start Date: June 18, 1969
End Date: June 20, 1969
Sponsors: CORNELL AERONAUTICAL LAB. AND U.S. ARMY AVIATION MATERIEL LABS.
Accession Number
69A35222
Distribution Limits
Public
Copyright
Other

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