THE EFFECT OF DISTRIBUTED SURFACE ROUGHNESS ON LAMINAR FLOW
作者： ALBERT E. VON DOENHOFF , ALBERT L. BRASLOW
DOI: 10.1016/B978-1-4832-1323-1.50005-1
关键词:
摘要: … concerns the effect of laminar stability on the lateral spread of … as increased laminar stability increases the extent of laminar … data on the effect of roughness on transi tion from laminar to …
sci-hub.se 参考文章(12)
Richard J Wisniewski, John R Jack, N S Diaconis, Boundary-layer Transition at Mach 3.12 as Affected by Cooling and Nose Blunting ,(1957)
E. R. VAN DRIEST, J. CHRISTOPHER BOISON, Experiments on Boundary-Layer Transition at Supersonic Speeds Journal of the Aeronautical Sciences. ,vol. 24, pp. 885- 899 ,(1957) , 10.2514/8.3994
HUGH L. DRYDEN, Review of Published Data on the Effect of Roughness on Transition from Laminar to Turbulent Flow Journal of the Aeronautical Sciences. ,vol. 20, pp. 477- 482 ,(1953) , 10.2514/8.2693
Albert L Braslow, Eugene C Knox, Simplified method for determination of critical height of distributed roughness particles for boundary-layer transition at Mach numbers from 0 to 5 ,(1958)
Milton A. Schwartzberg, Albert L. Braslow, Experimental study of the effects of finite surface disturbances and angle of attack on the laminar boundary layer of an NACA 64A010 airfoil with area suction ,(1952)
G. B. Schubauer, P. S. Klebanoff, Contributions on the Mechanics of Boundary-Layer Transition ,(1955)
DEAN R. CHAPMAN, MORRIS W. RUBESIN, Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature Journal of the Aeronautical Sciences. ,vol. 16, pp. 547- 565 ,(1949) , 10.2514/8.11853
Alvin Seiff, James R. Jedlicka, Max E. Wilkins, Experimental determination of boundary-layer transition on a body of revolution at M = 3.5 ,(1954)