论文信息 - Comparison of NASA 9x15 Low Speed Wind Tunnel Counter Rotating Open Rotor Data with GE-Anechoic Facility Historic Data for Baseline F31A31 Blade Design - 字舞流文

Comparison of NASA 9x15 Low Speed Wind Tunnel Counter Rotating Open Rotor Data with GE-Anechoic Facility Historic Data for Baseline F31A31 Blade Design

John Wojno | B. Janardan

[1] Gary G. Podboy,et al. Laser velocimeter measurements of the flowfield generated by an advanced counterrotating propeller , 1989 .

[2] C. Balan,et al. A model propulsion simulator for evaluating counter rotating blade characteristics , 1986 .

[3] B. A. Janardan,et al. Acoustic characteristics of counterrotating unducted fans from modelscale tests , 1990 .

[4] B. A. Janardan,et al. Scale model acoustic testing of counterrotating fans , 1988 .

[5] Richard P. Woodward,et al. An Open Rotor Test Case: F31/A31 Historical Baseline Blade Set , 2011 .

[6] David M. Elliott. Initial Investigation of the Acoustics of a Counter-Rotating Open Rotor Model with Historical Baseline Blades in a Low-Speed Wind Tunnel , 2013 .

[7] D. C. Wisler,et al. Rotor-rotor interaction for counter-rotating fans. I - Three-dimensional flowfield measurements , 1994 .

[8] Richard P. Woodward. Noise of two high-speed model counter-rotation propellers at takeoff/approach conditions , 1992 .

[9] B. Shivashankara,et al. Installation effects on counter rotating propeller noise , 1990 .