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Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions — ReaderExpo

Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions

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Flow structure generated by perpendicular blade vortex interaction and implications for helicopter noise predictions

by William J. Devenport

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Blade slap noiseBlade-vortex interactionHelicoptersNoise predictionRotary wingsWind tunnel tests

Keep the story going

Helicopter blade-vortex interaction noise with comparisons to CFD calculations

Megan S. McCluer

Reduction of Blade-Vortex Interaction (BVI) noise through X-force control

Fredric H. Schmitz

Evaluation of a doubly-swept blade tip for rotorcraft noise reduction

Brian E. Wake

UHB engine fan broadband noise reduction study

Philip R. Gliebe

The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction

William J. Devenport