Correlation of Theory to Wind-Tunnel Data at Reynolds Numbers below 500,000

Author:

Evangelista Raquel,McGhee Robert J.,Walker Betty S.

Publisher

Springer Berlin Heidelberg

Reference10 articles.

1. Eppler, R. and Somers, D. M., A Computer Program for the Design and Analysis of Low-Speed Airfoils., NASA TM 80210 (1980).

2. Eppler, R. and Somers, D. M., Supplement to: A Computer Program for the Design and Analysis of Low-Speed Airfoils., NASA TM 81862 (December 1980).

3. Drela, M., Two-Dimensional Aerodynamic Design and Analysis Using the Euler Equations., Massachusetts Institute of Technology, Gas Turbine Laboratory Rept. 187 (February 1986).

4. Drela, M. and Giles, M. B., Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils., AIAA Journal 25, No. 10, 1347–1355.

5. McGhee, R. J., Walker, B. S. and Millard, B. F., Experimental Results for the Eppler 387 Airfoil at Low Reynolds Numbers in the Langley Low-Turbulence Pressure Tunnel., NASA TM 4062 (October 1988).

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