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. Prandtl L. Über Reibungsschichten bei dreidimensionalen Strömungen. Festschrift zum 60. Geburtstage von A. Betz, Göttingen S. 134-141, 1945. (Ludwig Prandtl Gesammelte Abhandlungen, 2, 679-686, Springer-Verlag 1961).
Cooke JC. The boundary layer of a class of infinite yawed cylinders. Proc. Camb. Phil. Soc. 46, 645-648, 1950.
Cooke JC. Pohlhausen’s method for three-dimensional boundary layers. Aeronaut. Quart. 3, 51-60, 1951.
. Pfenninger W. Laminar flow control. AGARD Rep. No. 654 (Special course on drag reduction), VKI, Rhode-St.-Genese, Belg, 1977.
Reed HL, Saric WS, Arnal, D Linear Stability Theory Applied to Boundary Layers. Ann. Rev. Fluid Mech. 28, 389-428, 1996.
Saric WS, Reed HL, Kerschen EJ. Boundary-Layer Receptivity to Freestream Disturbances. Ann. Rev. Fluid Mech. 34, 291-319, 2002.
Saric WS, Reed HL, White EB. Stability and Transition of 3-D Boundary Layers. Ann. Rev. Fluid Mech. 35, 413-440, 2003.
Saric WS, Carillo RB, Reibert MS. Nonlinear stability and transition in 3-D boundary layers. Meccanica 33, 469-487, 1998.
Haynes T, Reed HL. Simulation of swept-wing vortices using nonlinear parabolized stability equations. J. Fluid Mech. 405, 325-349, 2000.
Wassermann P, Kloker M. Mechanisms and control of crossflowvortex induced transition in a 3-D boundary layer. J. Fluid Mech. 456, 49-84, 2002.
Saric WS. Görtler vortices. Ann. Rev. Fluid Mech. 26, 379-409, 1994.
Poll DIA. Some observations of the transition process on the windward face of a long yawed cylinder. J. Fluid Mech. 150, 329-56, 1985.
Reed HL, Saric WS. Stability of three-dimensional boundary layers. Ann. Rev. Fluid Mech. 21, 235-84, 1989.
. Reshotko E. 1984. Laminar Flow Control. In Special Course on Stability and Transition of Laminar Flows, AGARD Report 709.
. Reshotko E. Progress, accomplishments and issues in transition research. AIAA Pap. No. 1997-1815.
. Herbert T. Transition prediction and control for airplane applications. AIAA Pap. No. 1997-1908.
. Arnal D. Laminar-turbulent transition: Research and applications in France. AIAA Pap. No. 1997-1905.
Herbert, T. Parabolized stability equations. Ann. Rev. Fluid Mech. 29, 245-83, 1997.
. Bippes H. Environmental conditions and transition prediction in 3pD boundary layers. AIAA Pap. No. 1997p1906. 188 W .Saric and H .Reed
Bippes H. 1999. Basic experiments on transition in three- dimensional boundary layers dominated by crossflow instability. Prog. Aero. Sci. 35, 363-412.
. Crouch JD. Transition prediction and control for airplane applications. AIAA Pap. No. 1997-1907.
. Kachanov YS. Experimental studies of three-dimensional instability of boundary layer. AIAA Pap. No. 1996-1976.
. Saric WS, Carrillo RB, Reibert MS. Leading-edge roughness as a transition control mechanism. AIAA Pap. No. 1998-0781.
. Saric WS, Reed HL. Crossflow Instabilities - Theory and Technology. AIAA Paper No. 2003-0771.
. Kohama Y, Saric WS, Hoos JA. A high-frequency, secondary instability of crossflow vortices that leads to transition. In Proc. Royal Aero. Soc. Conf. on Boundary-Layer Transition and Control, 1991.
Malik MR, LF, Chang CL. Crossflow disturbances in three- dimensional boundary layers: Nonlinear development, wave interaction and secondary instability. J. Fluid Mech. 268, 1-36, 1994.
Malik MR, Li F, Choudhari MM, Chang CL. Secondary instability of crossflow vortices and swept-wing boundary layer transition. J. Fluid Mech. 399, 85-115, 1999
Janke E, Balakumar P. On the secondary instability of three- dimensional boundary layers. Theoret. Comput. Fluid Dyn. 14, 167-94, 2000.
. White EB, Saric WS. Secondary instability of crossflow vortices. In press J. Fluid Mech. 2004
Radeztsky RH Jr, Reibert MS, Saric WS. Effect of isolated micronsized roughness on transition in swept-wing flows. AIAA J. 37, 1371-7, 1999.
Deyhle H, Bippes H. Disturbance growth in an unstable threedimensional boundary layer and its dependence on initial conditions. J. Fluid Mech. 316, 73-113, 1996.
Reshotko E. Transient Growth - A factor in by-pass transition. Phys. Fluids 13, 1067, 2001.
. White EB, Reshotko E. Roughness induced transient growth in a flat-plate boundary layer. AIAA Paper No. 2002-0138.
Joslin RD. Aircraft laminar flow control. Ann. Rev. Fluid Mech. 30: 1-29, 1998.
. Saric WS, Reed HL. Supersonic laminar flow control on swept wings using distributed roughness. AIAA Pap. No. 2002-0147.
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Saric, W., Reed, H. (2006). Stability, Transition, and Control of Three-Dimensional Boundary Layers on Swept Wings. In: Meier, G.E.A., Sreenivasan, K.R., Heinemann, HJ. (eds) IUTAM Symposium on One Hundred Years of Boundary Layer Research. Solid mechanics and its applications, vol 129. Springer, Dordrecht. https://doi.org/10.1007/978-1-4020-4150-1_17
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