The Unsteady Boundary Layer in a Shock Tube
作者： B. E. L. Deckker , M. E. Weekes
DOI: 10.1243/PIME_PROC_1976_190_031_02
关键词:
摘要: SYNOPSIS The unsteady boundary layer behind a moving shock wave in rectangular duct 7.62 cm wide × 5.08 high has been studied using quality schlieren system. Growth of the compared with results calculations for laminar and turbulent flows. experimental indicate that three dimensional effects are present which cause, some cases, very early transition from to flow. Agreement theory is satisfactory only case weakest examined although trends growth rates generally conform theoretical predictions.
harvard.edu
sagepub.com
sci-hub.se 参考文章(7)
S. H. Lam, L. Crocco, Note on the Shock-Induced Unsteady Laminar Boundary Layer on a Semi-Infinite Flat Plate Journal of the Aerospace Sciences. ,vol. 26, pp. 54- 56 ,(1959) , 10.2514/8.7924
WAYLAND GRIFFITH, Shock-Tube Studies of Transonic Flow over Wedge Profiles Journal of the Aeronautical Sciences. ,vol. 19, pp. 249- 257 ,(1952) , 10.2514/8.2242
Che Jen Chen, Raymond J. Emrich, Investigation of the Shock‐Tube Boundary Layer by a Tracer Method Physics of Fluids. ,vol. 6, pp. 1- 9 ,(1963) , 10.1063/1.1724502
J. D. A. Walker And, S. C. R. Dennis, The boundary layer in a shock tube Journal of Fluid Mechanics. ,vol. 56, pp. 19- 47 ,(1972) , 10.1017/S0022112072002150
Edmund J. Gion, Measured Velocity Profiles in the Laminar Boundary Layer Behind a Shock Physics of Fluids. ,vol. 8, pp. 546- 547 ,(1965) , 10.1063/1.1761260
Herman Mark, Michael J. Mirtich, Transition in Shock‐Tube Boundary Layers Physics of Fluids. ,vol. 5, pp. 251- 253 ,(1962) , 10.1063/1.1706605
P. Bradshaw, D. H. Ferriss, N. P. Atwell, Calculation of boundary-layer development using the turbulent energy equation Journal of Fluid Mechanics. ,vol. 28, pp. 593- 616 ,(1967) , 10.1017/S0022112067002319