Low Reynolds Number Airfoil Design and Wind Tunnel Testing at Princeton University

Author:

Donovan J. F.,Selig M. S.

Publisher

Springer Berlin Heidelberg

Reference20 articles.

1. van Ingen, J. L. and Boermans, L. M. M., “Aerodynamics at Low Reynolds Numbers: A Review of Theoretical and Experimental Research at Delft University of Technology,” Aerodynamics at Low Reynolds Numbers 104 Re 106 International Conference, London, October 1986.

2. Dobbinga, E., van Ingen, J. L., and Kooi, J. W., “Some Research on Two-Dimensional Laminar Separation Bubbles,” AGARD CP-102, Paper 2, Lisbon, 1972.

3. Eppler, R. and Somers, D. M., “Airfoil Design for Reynolds Numbers Between 50,000 and 500,000,” Proceedings of the Conference on Low Reynolds Number Airfoil Aerodynamics, Notre Dame, Indiana, June 1986.

4. Eppler, R. and Somers, D. M., “A Computer Program for the Design and Analysis of Low-Speed Airfoils, Including Transition,” NASA TM 80210, August 1980.

5. Drela, M. and Giles, M. B., “Viscous-Inviscid Analysis of Transonic and Low-Reynolds Number Airfoils,” AIAA J., Vol. 25, No. 9, September 1987.

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