Comparison of NASA 9x15 low speed wind tunnel counter rotating open rotor data with GE-anechoic facility historic data for baseline F31A31 blade design

19th AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 2013, Pages 196-

  Wojno, J P ^a   Janardan, B A ^a  

^a GE AVIATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; AERODYNAMICS; FANS; NASA; OPEN DATA; SOFTWARE TESTING; TUNNELS; WIND TUNNELS;

AERO-DYNAMIC PERFORMANCE; BASELINE DATA; BLADE DESIGN; COLLABORATIVE PARTNERSHIPS; COUNTER ROTATING; HISTORIC DATA; LOW-SPEED WIND TUNNEL; SCALE MODELING;

TURBOMACHINE BLADES;

EID: 84881467598     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2013-2204     Document Type: Conference Paper

References (13)

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4. thAerodynamic Testing Conference, San Diego, CA, May 1988.
5. Hoff, G.E., et al., "Experimental Performance and Acoustic Investigation of Modern Counter-rotating Blade Concepts", NASA CR-185138, January 1990.
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10. thAerospace Sciences Meeting, Reno, NV, January 1989
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12. thAIAA/CEAS Aeroacoustics Conference, Portland, OR, June 2011
13. Van Zante, D.E., Gazzaniga, J.A., Elliott, D.M., and Woodward, R.P., "An Open Rotor Test Case: F31A31 Historical Baseline Blade Set", ISABE 2011-1310, International Society of Air Breathing Engine, Gothenburg, Sweden, Sept 2011.