Airframe noise modeling appropriate for multidisciplinary design and optimization

AIAA Paper

Volumn , Issue , 2004, Pages 8087-8098

  Hosder, Serhat ^a,b   Schetz, Joseph A ^a,b   Grossman, Bernard ^a,b,c   Mason, William H ^a,b  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

^b Department of Aerospace Engineering ^*  (United States)

^c NATIONAL INSTITUTE OF AEROSPACE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; AERODYNAMICS; AIRFOILS; AIRFRAMES; DRAG; KINETIC ENERGY; MATHEMATICAL MODELS; POLLUTION; REYNOLDS NUMBER; TURBULENCE; WINGS;

FREE-STREAM VELOCITY; NOISE INTENSITY; TURBULENCE FREQUENCY; WING SPAN;

AEROSPACE ENGINEERING;

EID: 2942741226     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-698     Document Type: Conference Paper

References (20)

1. NASA Aeronautics Blueprint: Toward a Bold New Era in Aviation. http://www.aerospace.nasa.gov/aero_blueprint/cover.html.
2. Antoine, N. E. and Kroo, I. M. "Aircarft Optimization For Minimal Environmental Impact", AIAA Paper 2002-5667, September 2002.
3. Aeronautics and Space Transportation Technology: Three Pillars for Success, Turning Goals Into Reality. NASA Annual Progress Report 1997-98.
4. Crighton, D. G. Airframe Noise (Chapter 7). In Aeroacoustics of Flight Vehicles: Theory and Practice, Volume 1: Noise Sources, pages 397-447. edited by Hubbard, H. H., NASA Reference Publication 1258, WRDC Technical Report 90-3052, 1991.
5. Lilley, G. M. "The prediction of Airframe Noise and Comparison with Experiment". Journal of Sound and Vibration, 239(4):849-859, 2001.
6. Ko, A., Leifsson, L. T., Schetz, J. A., Mason, W. H., Grossman, B., and Haftka, R. T. "MDO of a Blended-Wing-Body Transport Aircraft with Distributed Propulsion", AIAA Paper 2003-6732, November 2003.
7. Dippold, V. F., Hosder, S., and Schetz, J. A. "Analysis of Jet-Wing Distributed Propulsion From Thick Wing Trailing Edges", AIAA Paper 2004-1205, January 2004.
8. Goldstein, M. E. Aeroacoustics. McGraw-Hill Book Company, New York, 1976.
9. Lilley, G. M. "A Study of the Silent Flight of the Owl", AIAA Paper 1998-2340, 1998.
10. Howe M. S. "A Review of the Theory of Trailing Edge Noise". Journal of Sound and Vibration, 61(3):437-465, 1978.
11. Lighthill, M. J. On Sound Generated Aerody-namically. I. General Theory. In Proceedings of the Royal Society A211, pages 564-587. London, 1952.
12. Ffowcs Williams, J. E. and Hall, L. H. "Aerody-namic Sound Generation by Turbulent Flow in the Vicinty of a Scattering Half Plane". Journal of Fluid Mechanics, 40(4):657-670, March 1970.
13. Fink, M. R. Airframe Noise Prediction Method. Report No. FAA-RD-77-29, Federal Aviation Administration, March 1977.
14. Brooks, T. F., Pope, S. D., and Marcolini, M. A. "Airfoil Self-Noise and Prediction". NASA Reference Publication 1218, NASA Langley Research Center, July 1989.
15. Singer, B. A., Brentner, K. S., Lockard, D. P., and Lilley, G. M. "Simulation of Acoustic Scattering from a Trailing Edge", AIAA Paper 1999-0231, 1999.
16. GASP User Manual. AeroSoft, Inc., Blacksburg, Virginia, 1997.
17. Menter F. "Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications". AIAA Journal, 32:1598-1605, 1994.
18. Bardina, J. E., Huang, P. G., and Coakley, T. J. "Turbulence Modeling Validation", AIAA Paper 1997-2121, 1997.
19. Harris, C. D. "NASA Supercritical Airfoils A Matrix of Family Related Airfoils". NASA Technical Paper 2969, NASA Langley Research Center, 1990.
20. Jacobs, P. F. and Gloss, B. B. "Longitudinal Aerodynamic Characteristics of a Subsonic, Energy-Efficient Transport Configuration in the National Transonic Facility". NASA Technical Paper 2922, NASA Langley Research Center, 1989.