RCAIDE.Library.Methods.Noise.Frequency_Domain_Buildup.Rotor
Rotor#
RCAIDE Package Setup
Modules
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This computes the boundary layer properties using the method outlined by the Brooks, Pope and Marcolini (BPM) Model |
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This computes the laminar boundary layer compoment of broadband noise using the method outlined by the Brooks, Pope and Marcolini (BPM) Model |
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This computes the turbument boundary layer- trailing edge noise compoment of broadband noise using the method outlined by the Brooks, Pope and Marcolini (BPM) Model |
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This computes the tip noise compoment of broadband noise using the method outlined by the Brooks, Pope and Marcolini (BPM) Model |
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This computes the trailing edge noise compoment of broadband noise of a propeller or lift-rotor in the frequency domain. |
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This is a collection medium-fidelity frequency domain methods for rotor acoustic noise prediction which computes the acoustic signature (sound pressure level, weighted sound pressure levels, and frequency spectrums of a system of rotating blades |
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This computes the harmonic noise (i.e. thickness and loading noise) in the frequency domain of a rotor at any angle of attack with load distribution along the blade span. |
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This computes the harmonic noise (i.e. thickness and loading noise) in the frequency domain of a rotor at any angle of attack with load distribution along the blade span and blade chord. |
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This computes the harmonic noise (i.e. thickness and loading noise) in the frequency domain of a rotor at any angle of attack having the loads act at a single point. |
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This computes the laminar boundary layer compoment of broadband noise using the method outlined by the Brooks, Pope and Marcolini (BPM) Model |