Integrated Transition Prediction: A Case Study in Supersonic Laminar Flow Control

† Aerospace Technologist, Computational Modeling and Simulation Branch, Senior Member AIAA Email: m.m.choudhari@larc.nasa.gov †† Aerospace Technologist, Computational Modeling and Simulation Branch, Senior Member AIAA ††† Aerospace Technologist, Computational Modeling and Simulation Branch. * Aerospace Technologist, Flow Physics and Control Branch, Senior Member AIAA Copyright © 2003 by the American Institute of Aeronautics and Astronautics, Inc. No copyright is asserted in the United States under Title 17, U.S. Code. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental Purposes. All other rights are reserved by the copyright owner. Abstract

[1]  Dennis M. Bushnell Applications and suggested directions of transition research , 1990 .

[2]  Xiaolin Zhong,et al.  Direct numerical simulation of hypersonic boundary-layer transition over blunt leading edges. II - Receptivity to sound , 1997 .

[3]  Hans G. Hornung,et al.  Stabilization of Hypersonic Boundary Layers by Porous Coatings , 2001 .

[4]  J. A. Masad,et al.  Three-dimensional boundary-layer transition on a swept wing at Mach 3.5 , 1995 .

[5]  William S. Saric,et al.  Supersonic Laminar Flow Control on Swept Wings Using Distributed Roughness Stability Analysis and Computations , 2002 .

[6]  H. Bippes,et al.  Experimental Study of Instability Modes in a Three-dimensional Boundary Layer. , 1987 .

[7]  Meelan Choudhari,et al.  Secondary instability of crossflow vortices and swept-wing boundary-layer transition , 1999, Journal of Fluid Mechanics.

[8]  Alexander N. Shiplyuk,et al.  Hypersonic flow stability experiments , 2002 .

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

[10]  C. L. Streett Direct Harmonic Linear Navier-Stokes Methods for Efficient Simulation of Wave Packets , 1998 .

[11]  M. E. Goldstein,et al.  Scattering of acoustic waves into Tollmien-Schlichting waves by small streamwise variations in surface geometry , 1985, Journal of Fluid Mechanics.

[12]  William S. Saric,et al.  Leading-Edge Roughness as a Transition Control Mechanism , 1998 .

[13]  William S. Saric,et al.  Boundary-layer receptivity of sound with roughness , 1991 .

[14]  J. D. Crouch,et al.  Transition Prediction and Control for Airplane Applications , 1997 .

[15]  Peter A. Monkewitz,et al.  Subharmonic resonance, pairing and shredding in the mixing layer , 1988, Journal of Fluid Mechanics.

[16]  A. Shiplyuk,et al.  Leading-edge receptivity of a hypersonic boundary layer on a flat plate , 2001, Journal of Fluid Mechanics.

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

[18]  Meelan Choudhari Boundary-layer receptivity due to distributed surface imperfections of a deterministic or random nature , 1992 .

[19]  Eli Reshotko,et al.  BOUNDARY LAYER STABILITY AND TRANSITION , 1976 .

[20]  M. Malik,et al.  Hypersonic Boundary-Layer Stability with Chemical Reactions using PSE , 1997 .

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

[22]  A. Ruban On the generation of Tollmien-Schlichting waves by sound , 1984 .

[23]  Chau-Lyan Chang,et al.  The Langley Stability and Transition Analysis Code (LASTRAC) : LST, Linear and Nonlinear PSE for 2-D, Axisymmetric, and Infinite Swept Wing Boundary Layers , 2003 .

[24]  Mujeeb R. Malik,et al.  Boundary-Layer Transition Prediction Toolkit , 1997 .

[25]  Scott G. Anders,et al.  F-16XL-2 Supersonic Laminar Flow Control Flight Test Experiment , 1999 .

[26]  Yong-Sun Wie,et al.  BLSTA: A boundary layer code for stability analysis , 1992 .

[27]  Li Jiang,et al.  Cross-validation of DNS and PSE results for instability wave propagation in compressible boundary layers past curvilinear surfaces , 2003 .

[28]  Xuesong Wu,et al.  Generation of Tollmien–Schlichting waves by convecting gusts interacting with sound , 1999, Journal of Fluid Mechanics.

[29]  Erik Janke,et al.  Transition Control using Leading Edge Roughness , 1999 .

[30]  Ilan Kroo,et al.  Natural Laminar Flow for Quiet and Efficient Supersonic Aircraft , 2002 .

[31]  Receptivity to surface roughness near a swept leading edge , 1999 .

[32]  Erik Janke,et al.  Receptivity and transition control of swept-wing boundary layers; Effects of surface curvature and nonlinearity , 2001 .

[33]  William S. Saric,et al.  Review of Swept-Wing Transition , 1997 .

[34]  E. Reshotko Boundary layer instability, transition and control , 1994 .

[35]  L. Veitch,et al.  Quiet Supersonic Platform Program Advanced algorithms for design and optimization of Quiet Supersonic Platforms , 2002 .

[36]  J. D. Crouch,et al.  Roughness-induced receptivity to crossflow vortices on a swept wing , 1999 .

[37]  William S. Saric,et al.  Forced and unforced subharmonic resonance in boundary-layer transition , 1984 .

[38]  Helen L. Reed,et al.  Computational Fluid Dynamics Validation Issues in Transition Modeling , 1998 .

[39]  Craig L. Streett,et al.  Boundary layer receptivity phenomena in three-dimensional and high-speed boundary layers , 1990 .

[40]  Craig L. Streett,et al.  Theoretical prediction of boundary-layer receptivity , 1994 .

[41]  Alexander Fedorov,et al.  Excitation of unstable modes in a supersonic boundary layer by acoustic waves , 1991 .

[42]  S. Scott Collis,et al.  Adjoint parabolized stability equations for receptivity prediction , 2000 .

[43]  M. Y. Hussaini,et al.  Compressible stability of growing boundary layers using parabolized stability equations , 1991 .

[44]  Craig Streett Designing a Hybrid Laminar-Flow Control Experiment via CFD (Invited) , 2003 .

[45]  Craig L. Streett,et al.  Simulation of crossflow instability on a supersonic highly swept wing , 2000 .

[46]  Helen L. Reed,et al.  Computations in nonlinear saturation of stationary crossflow vortices in a swept-wing boundary layer , 1996 .