Modeling Transition Physics for Laminar Flow Control

*Laminar flow control requires transition-prediction methods that can account for the varied surface-quality and free-stream environmental conditions encountered during implementation or development. A variable N-factor transition-prediction scheme is presented, which accounts for many of the physical mechanisms important for the practical applications of laminar flow. The approach is based on correlations with linear instability amplification factors (n-factors), but also draws on receptivity theory and growth modifiers. For external factors that are not accommodated within the variable N-factor framework, other empirical-correlation models are considered.

[1]  J. V. Ingen A suggested semi-empirical method for the calculation of the boundary layer transition region , 1956 .

[2]  L. Mack,et al.  Stability of Three-Dimensional Boundary Layers on Swept Wings at Transonic Speeds , 1989 .

[3]  E. Reshotko,et al.  Preliminary Experimental Study of Disturbances in a Laminar Boundary- Layer due to Distributed Surface Roughness , 1981 .

[4]  F. S. Collier,et al.  An overview of recent subsonic laminar flow control flight experiments , 1993 .

[5]  Edward B. White,et al.  RECEPTIVITY AND TRANSIENT GROWTH OF ROUGHNESS-INDUCED DISTURBANCES , 2003 .

[6]  J. E. Ffowcs Williams,et al.  Transition from laminar to turbulent flow , 1969, Journal of Fluid Mechanics.

[7]  T. Herbert PARABOLIZED STABILITY EQUATIONS , 1994 .

[8]  Mark V. Morkovin,et al.  On Roughness — Induced Transition: Facts, Views, and Speculations , 1990 .

[9]  H. Deyhle,et al.  Disturbance growth in an unstable three-dimensional boundary layer and its dependence on environmental conditions , 1996, Journal of Fluid Mechanics.

[10]  L. Mack,et al.  Transition prediction and linear stability theory , 1977 .

[11]  C. S. Wells Effects of freestream turbulence on boundary- layer transition. , 1967 .

[12]  M. V. Morkovin,et al.  Experiments on transition enhancement by distributed roughness , 1986 .

[13]  J. D. Crouch,et al.  Variable N-Factor Method for Transition Prediction in Three-Dimensional Boundary Layers , 2000 .

[14]  J. Crouch,et al.  Receptivity of three-dimensional boundary layers , 1993 .

[15]  J. Crouch,et al.  Theoretical studies on the receptivity of boundary layers , 1994 .

[16]  J. D. Crouch,et al.  MODELING THE EFFECTS OF STEPS ON BOUNDARY-LAYER TRANSITION , 2006 .

[17]  J. Crouch Receptivity Issues for Laminar-Flow Control , 1999 .

[18]  Meelan M. Choudhari,et al.  Roughness-induced generation of crossflow vortices in three-dimensional boundary layers , 1994, Theoretical and Computational Fluid Dynamics.

[19]  William S. Saric,et al.  Effect of micron-sized roughness on transition in swept-wing flows , 1993 .

[20]  Albert L. Braslow,et al.  THE EFFECT OF DISTRIBUTED SURFACE ROUGHNESS ON LAMINAR FLOW , 1961 .

[21]  Michimasa Fujino,et al.  Natural-Laminar-Flow Airfoil Development for a Lightweight Business Jet , 2003 .

[22]  P. Spalart,et al.  Linear and nonlinear stability of the Blasius boundary layer , 1992, Journal of Fluid Mechanics.

[23]  D Joslin Ronald,et al.  Aircraft Laminar Flow Control , 1998 .

[24]  Y. X. Wang,et al.  Effect of surface steps on boundary layer transition , 2005 .

[25]  P. Fischer,et al.  ROUGHNESS INDUCED TRANSIENT GROWTH: NONLINEAR EFFECTS , 2006 .

[26]  H. L. Dryden A. Transition from Laminar to Turbulent Flow , 1960 .