Acoustics
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Can Shock Waves on Helicopter Rotors Generate Noise? A Study of Quadrupole Source Member price: $15.00 $30.00
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The Acoustic Results of a United Technologies Scale Model Helicopter Rotor Tested at DNW Member price: $15.00 $30.00
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Prediction of Blade-Vortex Interaction Noise Using Airloads Generated by a Finite-Difference Technique Member price: $15.00 $30.00
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Three-Dimensional Shock Fitting for Transonic Rotor Acoustics Member price: $15.00 $30.00
