RCAIDE.Library.Methods.Noise.Correlation_Buildup.Airframe
Airframe#
RCAIDE Package Setup
Modules
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This computes the noise from different sources of the airframe for a given vehicle for a constant altitude flight. |
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This computes the 1/3 octave band sound pressure level and the overall sound pressure level from the clean wing, for a wing with area S (sq.ft) and span b (ft). |
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This calculates the Landing gear 1/3 octave band sound pressure level and overall sound pressure level for a tyre diameter D, a strut length H and WHEELS number of wheels per unit. |
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This calculates the noise from the flap trailing edge as a 1/3 octave band sound pressure level. |