Open rotor designs for low noise and high efficiency

Proceedings of the ASME Turbo Expo

Volumn 6 C, Issue , 2013, Pages

  Khalid, S Arif ^a   Wojno, John P ^a   Breeze Stringfellow, Andy ^a   Lurie, David P ^a   Wood, Trevor H ^b   Ramakrishnan, Kishore ^b   Paliath, Umesh ^b  

^a GE AVIATION   (United States)

^b GE GLOBAL RESEARCH   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AEROACOUSTICS; COMPUTATIONAL FLUID DYNAMICS; EFFICIENCY; FIGHTER AIRCRAFT; NASA; PROPULSION; SOFTWARE TESTING; WIND TUNNELS;

COMMUNITY NOISE; COST-SHARE PROGRAMS; DESIGN PHASE; FLIGHT SPEED; HIGHER EFFICIENCY; LOW-HIGH; LOWER NOISE; NARROW BODY AIRCRAFTS; OPEN ROTORS; ROTOR DESIGN;

PROPELLERS;

EID: 84890134696     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2013-94736     Document Type: Conference Paper

References (13)

1. Sullivan, T. J., "Aerodynamic Performance of a Scale- Model, Counterrotating Unducted Fan, " ASME Journal of Turbomachinery, vol. 112, pp. 579-586, 1990.
2. Guynn, Mark D., Berton, Jeffrey J., Haller, William J., Hendricks, Eric S., and Tong, Michael T., "Performance and Environmental Assessment of an Advanced Aircraft with Open Rotor Propulsion, " NASA/TM-2012-217772, NASA Langely Research Center, Hampton, VA, 2012.
3. Stefko, G. L. and Jeracki, R. J., "Porous Wind Tunnel Corrections for Counterrotation Propeller Testing, " NASA/TM-100873, 1988.
4. Gliebe, Philip R., "Flight Test vs. Model Test UDF® Engine Noise, " in Royal Aeronautical Society Conference, Advanced Propellers and their Installation on Aircraft, Cranfield Institute of Technology, England, Sept. 26-27, 1988.
5. Smith, L. H., "Unducted Fan Aerodynamic Design, " ASME Journal of Turbomachinery, vol. 109, pp. 313-324, 1987.
6. Smith, A. M. O. and Pierce, J., "Exact Solution of the Neumann Problem, Calculation of Non-circulatory Plane and Axially Symmetric Flows About or Within Arbitrary Boundaries, " Douglas Aircraft, Report No. ES 26988, 1958.
7. Hess, J. L. and Smith, A. M. O., "Calculation of Nonlifting Potential Flow About Arbitrary Three Dimensional Bodies, " Douglas Aircraft, Report No. ES 40622, 1962.
8. Sharma, A. and Chen, H., "Prediction of Tonal Aerodynamic Noise from Open Rotors, " in 18th AIAA/CEAS Aeroacoustics Conference, AIAA-2012-2265, Colorado Springs, CO, 2012.
9. Metzger, F. B. and Brown, P. C., "Results of Acoustic Tests of a Prop-Fan Model, " in AIAA/SAE/ASME/ASEE 23rd Joint Propulsion Conference, AIAA-87-1894, San Diego, CA, 1984.
10. Magliozzi, B., "Noise Characteristics of a Model Counterrotating Prop-Fan, " in 11th AIAA Aeroacoustics Conference, AIAA-87-2656, Sunnyvale, CA, 1987.
11. Elliott, David M., "Initial Investigation of the Acoustics of a Counter Rotating Open Rotor Model With Historical Baseline Blades in a Low Speed Wind Tunnel, " in 17th AIAA/CEAS Aeroacoustics Conference, AIAA 2011-2760, Portland, OR, 2011.
12. Van Zante, Dale, Gazzaniga, John, Eliott, David, and Woodward, Richard, "An Open Rotor Test Case: F31/A31 Historical Baseline Blade Set, " in ISABE-2011-1310, Gothenburg, Sweden, 2011.
13. Majjigi, Muni and Wojno, John P., "Previous Open Rotor Noise Experience at GE, " in X-Noise Open Rotor Technology Seminar, Lausanne, Switzerland, 18 March, 2011, pp. 1-8.