A TECHNIQUE FOR THE PREDICTION OF PROPELLER INDUCED ACOUSTIC LOADS ON AIRCRAFT STRUCTURES
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[1] F. H. Schmitz,et al. Transonic rotor noise: Theoretical and experimental comparisons , 1980 .
[2] Richard P. Woodward,et al. Measured noise of a scale model high speed propeller at simulated takeoff/approach conditions , 1987 .
[3] R. Srivastava,et al. Application of an efficient hybrid scheme for aeroelastic analysis of advanced propellers , 1990 .
[4] F. Farassat,et al. Quadrupole source in prediction of the noise of rotating blades - A new source description , 1987 .
[5] Peter Bushnell. Measurement of the steady surface pressure distribution on a single rotation large scale advanced prop-fan blade at Mach numbers from 0.03 to 0.78 , 1988 .
[6] D. B. Hanson,et al. The importance of quadrupole sources in prediction of transonic tip speed propeller noise , 1978 .
[7] F. Farassat,et al. The Uses and Abuses of the Acoustic Analogy in Helicopter Rotor Noise Prediction , 1987 .
[8] A third order upwind scheme for aero-acoustic applications , 1993 .
[9] A. Fuhs. Real gas effects in compressors for aircraft gas turbines , 1971 .