Errata: Prediction of Turbulent Boundary Layers at Low Reynolds Numbers

Abstract

Fig. 2 Vorticity of trailing vortex measured by vorticity meter. bulence, Rept. 74-01, Feb. 1974, Rochester Applied Science Associates, Rochester, N.Y. Poppleton, E.D., Preliminary Experimental of the of a Turbulent Trailing Vortex, TN 71-1, May 1971, McGill University, Montreal, Canada. Kantha, H.L., Lewellen, W.S., and Durgin, F.H., Qualitative Responses of a Core to Tip Blowing and Intersecting Airfoils, ASRL-TR 153-4, Aug. 1971, Massachusetts Institute of Technology, Cambridge, Mass. McCormick, B.W., Tangier, J.L., and Sherrieb, H.E., Structure of Trailing Vortices, Journal of Aircraft, Vol. 5, March 1968, p. 260. 5 White, R.P. and Balcerak, J.C., Investigation of the Dissipation of the Tip of a Rotor Blade by Mass Injection, TR 72-43, 1972, USAAMRDL, Ft. Eustis, Va., 1972. Sheath, D.D., Vortex Airfoil Interaction Tests, Proceedings of the AIAA 2nd Atmospheric Flight Mechanics Conference, Sept. 1972, Palo Alto, Calif. Corsiglia, V.R., Schwind, P.G., and Chigier, N.A., Rapid Scanning, Three-Dimensional, Hot-Wire Anemometer Surveys for Wing Tip Vortices in the Ames 40-by 80-Foot Wind Tunnel, AIAA Paper 73-629, Palm Springs, Calif., 1973. Orloff, K.L. and Grant, G.R., The Application of A Scanning Laser Doppler Velocimeter to Trailing Definition and Alleviation, AIAA Paper 73-680, Palm Springs, Calif., 1973. Marchman, J.F., III and Uzel, J.N., Effect of Several Wing Tip Modifications on a Trailing Vortex, Journal of Aircraft, Vol. 9, Sept. 1972, pp. 684-686.