Aerodynamic performance of scale-model turbofan outlet guide vanes designed for low noise

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Hughes, Christopher E ^a  

^a NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894372045     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

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2. Envia, E., "Fan Noise Reduction: An Overview, " NASA/TM-2001-210699, AIA A-2001-0661, 2001.
3. Bridges, J., Envia, E., and Huff, D., "Recent Developments in U.S. Engine Noise Reduction Research, " N AS A/TM-2001-211083, ISABE-2001-1017,2001.
4. Podboy, G., Krupar, M., Helland, S., and Hughes, C., "Measurements of the Flow Within a NASA 22 Inch Fan Model, " AIAA-2002-1033.
5. Yuska, J.A., Diedrich, J.H., and Nestor, C., "Lewis 9-by-15-Foot V/STOL Wind Tunnel, " NASA TMX-2305, 1971.
6. Arlington, A.E., and Gonsalez, J.C., "Flow Quality Improvements in the NASA Lewis Research Center 9-by 15-Foot Low Speed Wind Tunnel, " NASA CR-195439, 1995.
7. Dahl, M.D. and Woodward, R.P., "Acoustical Evaluation of the NASA Lewis 9-By 15-Foot Low Speed Wind Tunnel, " NASA TP-3274, 1992.
8. Balan, C. and Hoff, G.E., "Propulsion Simulator for High Bypass Turbofan Performance Evaluation, " SAE 931410, 1993.
9. Envia, E. and Nallasamy, M., "Design Selection and Analysis of a Swept and Leaned Stator Concept, " NASA/TM-1998-208662, 1998, Journal of Sound and Vibration, vol. 228, pp. 793-836, 1999.
10. Woodward, R.P., Elliot, D.M., Hughes, C.E., and Berton, J.J., "Benefits of Swept and Leaned Stators for Fan Noise Reduction, " NASA/TM-1998-208661, AIAA-99-0479, AIAA Journal of Aircraft, vol. 38, no. 6, 2001.