Inverse airfoil design using optimization

14th Applied Aerodynamics Conference

Volumn , Issue , 1996, Pages 1002-1010

  Venkataraman, P ^a  

^a Rochester Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; BOUNDARY LAYERS; DESIGN; GEOMETRY;

BOUNDARY LAYER DEVELOPMENT; DESIGN OBJECTIVES; DESIGN VARIABLES; FLIGHT CONDITIONS; INVERSE AIRFOIL DESIGN; MANUFACTURING CONSTRAINT; OPTIMIZATION METHOD; PARAMETRIC CURVE;

INVERSE PROBLEMS;

EID: 84964253346     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)

1. Venkataraman, P., Optimal Airfoil Design in Viscous Flows, Paper 95-1876, AIAA 13th Applied Aerodynamics conference, San Diego, CA 1995.
2. Venkataraman, P., Optimal Airfoil Design, Paper PS-IS? 1, AIAA 14th Applied Aerodynamics Conference, New Orleans, LA 1996.
3. Liebeck, R.H., and Ormsbee, R.H Optimization of Airfoils for Maximum Lift, Journal of Aircraft, Vol. 7, No. 5, 1969.
4. Miley, S.J., On the Design of Airfoils for Low Reynolds Number, Proceedings of the AIAA/MIT/SSA Second International Symposium of the Technology and Science of Low-Speed and Motorless Flight, Soaring Society of America, Los Angeles, CA 1974.
5. Selig, M.S., and Maughmer, M.D., Generalized Multipoint Inverse Airfoil Design, AIAA Journal, Vol. 30, No. 11, Nov. 1992.
6. Vanderplaats G.N., Hicks, R.N., and Murman, E.M., Applications of Numerical Optimization Technique to Airfoil Design, NASA Ames Research Center, NASA SP-347, Part II, pp 749-768, March 1975.
7. Venkataraman, P., A New Procedure for Airfoil Definition, Paper 95-1875, AIAA 13th Applied Aerodynamics Conference, San Diego, CA 1995.
8. Parkinson, et al., OptdesX - A Software Systemfor Optimal Engineering Design, Design Synthesis Inc., Provo, Utah, 1992.
9. Moran, J., An Introduction to Theoretical and Computational Aerodynamics, John Wiley and Sons, 1984.
10. Liebeck, R.H., Subsonic Airfoil Design, pg. 133-168, Applied Computational Aerodynamics, Ed. Progress in Astronautics and Aeronautics, AIAA, Vol. 125, 1990
11. Liebeck, R.H., and Camacho P. P., Airfoil Design at Low Reynolds Number with Constrained Pitching Moment, Proceedings of the Conference on Low Reynolds Number Aerodynamics, Ed. Thomas J. Mueller, University of Notre Dame, Indiana, 1985.
12. Drela, M., Elements of Airfoil Design Methodology, pplied Computational Aerodynamics, Ed. P.A.Henne, Progress in Astronautics and Aeronautics, AIAA, Vol. 125, 1990.