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Effects of ambient conditions on helicopter rotor source noise modeling
Eric Greenwood
, Fredric H. Schmitz
Aerospace Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
10
Scopus citations
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Dive into the research topics of 'Effects of ambient conditions on helicopter rotor source noise modeling'. Together they form a unique fingerprint.
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Keyphrases
Ambient Conditions
100%
Helicopter
100%
Helicopter Rotor
100%
Source Noise
100%
Noise Modeling
100%
Air Speed
33%
Advance Rate
33%
Rotor Harmonics
33%
Blade-vortex Interaction Noise
33%
External Noise
33%
Harmonic Noise
33%
True Airspeed
33%
Noise Level
16%
Rotorcraft
16%
Speed of Sound
16%
Modeling Method
16%
Directivity
16%
Main Rotor
16%
Helicopter Rotor Noise
16%
Thickness Noise
16%
Flight Condition
16%
Noise Estimation
16%
Bell
16%
Land Use Planning
16%
Noise Generation
16%
Acoustic Modeling
16%
Performance Equation
16%
Acoustic Equation
16%
Parameter Identification Method
16%
Flight Procedure
16%
Single-rotor Helicopter
16%
Noise Source Models
16%
Engineering
Ambient Condition
100%
Helicopter Rotors
100%
Noise Source
100%
Blade Vortex Interaction
66%
Rotors
33%
Noise Level
33%
Rotorcraft
33%
Directivity
33%
Main Rotor
33%
Flight Condition
33%
Thickness Noise
33%
Land Use
33%
Source Model
33%