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A parameter identification method for helicopter noise source identification and physics-based semiempirical modeling
Eric Greenwood
, Fredric H. Schmitz
Aerospace Engineering
Research output
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Contribution to journal
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Article
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peer-review
12
Scopus citations
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Dive into the research topics of 'A parameter identification method for helicopter noise source identification and physics-based semiempirical modeling'. Together they form a unique fingerprint.
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Keyphrases
Operating Conditions
100%
Noise Source
100%
Physics-based
100%
Noise Measurement
100%
Rotor Harmonics
100%
Helicopter Noise
100%
Noise Source Identification
100%
Semi-empirical Modeling
100%
Interaction Noise
100%
Parameter Identification Method
100%
Harmonic Noise
100%
Simulation Techniques
50%
Acoustics
50%
Wind Tunnel Test
50%
Condition-dependent
50%
Main Rotor
50%
Governing Parameters
50%
Individual Identification
50%
Bladed Rotor
50%
New Physics
50%
Two-bladed
50%
Number of Measurements
50%
Engineering
Rotors
100%
Noise Source
100%
Main Rotor
33%
Measurement Noise
33%
Simulation Technique
33%
Tunnel
33%
Physics
Harmonics
100%
Physics
100%
Wind Tunnels
50%
Noise Measurement
50%