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Geometry Considerations for Jet Noise Shielding with CTOL EngineOver-the-Wing Concept. AIAA 74-568
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von Glahn, U., Groesbeck, D., and Reshotko, M., "Geometry Considerations for Jet Noise Shielding with CTOL EngineOver-the-Wing Concept. AIAA 74-568, " 7th AIAA Fluid and Plasma Dynamics Conference, Palo Alto, California, USA, June 17-19, 1974.
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Validity of the Point Source Assumption in Rotor Noise Measurements with Shielding. AIAA 2010-3853
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Background Noise Levels Measured in the NASA Lewis 9-by 15-Foot Low-Speed Wind Tunnel. AIAA 95-0720
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Empennage Noise Shielding Benefits for an Open Rotor Transport
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Portland, Oregon, USA, 5-8 June
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Acoustic Characteristics of Counterrotating Fans from Model Scale Tests. AIAA 1989-1142
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San Antonio, Texas, USA, April 10-12
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Noise of Two High-Speed Model Counter-Rotation Propellers at Takeofi/Approach Conditions
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Initial Investigation of the Acoustics of a Counter Rotating Open Rotor Model with Historical Baseline Blades in a Low Speed Wind Tunnel
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A review of commonly used analytical and empirical formulae for predicting sound diffracted by a thin screen
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