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Helicopter Main-rotor Speed Effects on Far-field Acoustic Levels
Language: en
Pages: 24
Authors:
Categories:
Type: BOOK - Published: 1987 - Publisher:

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Helicopter Far-Field Acoustic Levels as a Function of Reduced Main-Rotor Advancing Blade-Tip Mach Number
Language: en
Pages: 32
Authors: National Aeronautics and Space Administration (NASA)
Categories:
Type: BOOK - Published: 2018-07-05 - Publisher: Createspace Independent Publishing Platform

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During the design of a helicopter, the weight, engine, rotor speed, and rotor geometry are given significant attention when considering the specific operations
Helicopter Impulsive Noise: Theoretical and Experimental Status
Language: en
Pages: 110
Authors: F. H. Schmitz
Categories:
Type: BOOK - Published: 1983 - Publisher:

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The theoretical and experimental status of helicopter impulsive noise is reviewed. The two major source mechanisms of helicopter impulsive noise are addressed:
Scientific and Technical Aerospace Reports
Language: en
Pages: 1572
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1992 - Publisher:

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