DTIC ADA156047: Aerodynamics and Acoustics of Propellers pdf

DTIC ADA156047: Aerodynamics and Acoustics of Propellers

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Particle contents: Design Concept and Performance Prediction Technique for Potential Flows around Advanced Propellers; Propeller Aerodynamic Prediction Methods; Aerodynamics of Wide-chord Propellers in Non-axisymmetric Flow; A Unified Approach for the Aerodynamics and Acoustics of Propellers in Forward Motion; Theoretical Analysis of Linearized Acoustics and Aerodynamics of Advanced Supersonic Propellers; A General Theory of Arbitrary Motion Aerodynamics Using an Aeroacoustic Approach; Recent NASA Propeller Research; An Asymptotic Theory for the Inference of Large Aspect Ratio Swept Wings and Multiple Propeller Slipstreams; Aeroacoustic Wind Tunnel Measurements on Propeller Noise; An Investigation of In-flight Near-field Propeller Noise Generation and Transmission; Propeller Aircraft Cabin Vibration and Noise- excitation Sources and Paths; Application of Active Noise Control to Model Propeller Noise

• Creator/s: Defense Technical Information Center
• Date: 2/1/1985
• Year: 1985
• Book Topics/Themes: DTIC Archive, , ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE), *ACOUSTICS, *AERIAL PROPELLERS, *AERODYNAMICS, *PROPELLER NOISE, AERODYNAMIC CHARACTERISTICS, AERODYNAMIC NOISE, EXCITATION, INFLIGHT, LINEARITY, MEASUREMENT, NEAR FIELD, NOISE, NOISE REDUCTION, POTENTIAL FLOW, PROPELLERS, SLIPSTREAM, SOUND TRANSMISSION, SUPERSONIC CHARACTERISTICS, SWEPT WINGS, SYMPOSIA, THEORY, VIBRATION, WIDTH, WIND TUNNEL TESTS

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