1. Sudani, N., Kanda, H., Sato, M., Miwa, H., Matsuno, K., and Takanashi, S., Evaluation of NACA0012 Airfoil Test Results in the NAL Two-Dimensional Transonic Wind Tunnel, NAL TR-1109T, Tokyo, (1991).
2. Barnwell, R. W., A Similarity Rule for Compressibility and Sidewall-Boundary-Layer, AIAA paper 79-0108, New Orleans, (1979).
3. Sewall, W. G., Effects of Sidewall Boundary Layers in Two-Dimensional Subsonic and Transonic Wind Tunnels, AIAA J., Vol. 20, No. 9, (1982) pp. 1253–1256.
4. Murthy, A. V., Effects of Aspect Ratio and Sidewall Boundary-Layer in Airfoil Testing, J. Aircraft, Vol. 25, No. 3, (1988) pp. 244–249.
5. Cook, W. J., Shock Tube as a Device for Testing Transonic Airfoils at High Reynolds Numbers, AIAA J., Vol. 17, No. 7, (1979) pp.715–721.