Design of minimum drag bodies in incompressible laminar flow

References

• Baldwin , B. S. and Lomax , H. Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows . AIAA 16th Aerospace Sciences Meeting . Jan , Huntsville. pp. 16 – 18 . Alahama
   Google Scholar
• Braza , M. , Chassaingh , P. and Minh , H. H. 1986 . Numerical Study and Physical Analysis of the Pressure and Velocity Fields in the Near Wake of a Circular Cylinder . J. Fluid Mech. , 165 : 79 – 130 .
   Google Scholar
• Burgreen , G. and Baysal , O. Three-Dimensional Aerodynamic Shape Optimization fo Wings Using Sensitivity Analysis . AIAA 32nd Aerospace Sciences Meeting & and Exhibit . Jan , Reno. pp. 10 – 13 . Nevada AIAA 94-0094
   Google Scholar
• Çabuk , H. , Sung , C. and Modi , V. 1992 . Explicit Runge-Kutta Method for Three-Dimensional Internal Imcompressible Flows . AIAA Journal , 30 : 2024 – 2031 .
   Google Scholar
• Çabuk , H. and Modi , V. 1992 . Optimum Plane Diffusers in Laminiar Flow . J. Fluid. Mech. , 237 : 373 – 393 .
   Google Scholar
• Dennis , S. C. R. and Chang , G. -Z. 1970 . Numerical Solution for Steady Flow Past a Circular Cylinder at Reynolds Numbers up to 100 . J. Fluid Mech , 42 : 471 – 489 .
   Google Scholar
• Dierckx , P. 1993 . Curve and Surface Fitting with Splines , 43 – 44 . New York : Oxford .
   Google Scholar
• Dulikravich , G. S. 1992 . Aerodynamic Shape design and Optimization: Status and Trends . J. Aircraft , 29 : 1020 – 1026 .
   Google Scholar
• Eleshaky , M. and Baysal , O. Design of 3-D Nacelle Near Flat-Plate Wing Using Multiblock Sensitivity Analysis (ADOS) . 32nd Aerospace Sciences Meeting & Exhibit . Jan 10–13 , Reno. NV AIAA Papper 94–0160
   Google Scholar
• Fornberg , B. 1980 . A Numerical Study of Steady Viscous Flow Past a Circular Cylinder . J. Fluid Mech. , 98 : 819 – 855 .
   Google Scholar
• Ganesh , Ram K. 1994 . The minimum Drag Profile in Laminar Flow: A Numerical Way . J. of Fluids Engineering. , 116 : 459 – 462 .
   Google Scholar
• Garabedian , P. and McFadden , G. B. 1982 . “ Computational Fluid Cynamics of Airfoils and Wings ” . In Proc. of Symposium and Transonic, Shock, and Multidimensional Flows, Madison 1981 , Edited by: Meyer , R. 1 – 16 . New York : Academic Press .
   Google Scholar
• Glowinski , R. and Pironneau , O. 1975 . On the Numecial Computation of the Minimum Drag Profile in Laminar Flow . J. Fluid. Mech. , 72 : 385 – 389 .
   Google Scholar
• Grove , A. S. , Shair , I. A. and Petersen , E. E. 1964 . An Experimental Investigation of the Steady Separated Flow Past a Circular Cylinder . J. Fluid Mech. , 9 : 60 – 80 .
   Google Scholar
• Han , T. , Hammond , D. C. and Sagi , C. J. 1992 . Optimization of Bluff Body for Minimum Drag in Ground Proximity . AIAA Journal , 30 : 82 – 889 .
   Google Scholar
• Hicks , R. M. and Henne , P. A. 1979 . Wing Design by Numerical Optimization AIAA Paper 79-0080
   Google Scholar
• Hirsch , C. 1990 . Numerical Computation of Internal and External Flows , Vol. 2 , 603 New York : John Wiley .
   Google Scholar
• Huan , J. and Modi , V. 1979 . Optimum Design of Drag Minimizing Bodies in Incompressible Flow . Inverse Problems in Engineering , 1 : 1 – 25 .
   Google Scholar
• Huan , J. 1995 . Design of Minimum Drag Bodies in Incompressible Flow Using an Optimal Control Approach , Columbia University . Ph. D. Dissertation
   Google Scholar
• Jacobs , E. N. and Abbott , I. H. 1939 . “ Airfoil Section Data Obtained in the N. A. C. A. Variable-Density Tunnel as Affected by Support Interference and other Corrections ” . In N. A. C. A. Twenty-fifth Annual Report 1939 507 – 538 .
   Google Scholar
• Jameson , A. 1988 . “ Aerodynamic Design via Control Theory ” . In ICASE Report No. 88–64 , NASA Langley Research Center .
   Google Scholar
• Kreiss , H.-O. and Lorenz , J. 1989 . Initial-Boundary Value Problems and the Navier-Stokes Equations , 347 – 349 . New York : Academic Press .
   Google Scholar
• Labrujère , Th. E. and Sloof , J. W. 1993 . Computational Methods for the Aerodynamic Design of Aircraft Components . Annual Review of Fluid Mechanics , 25 : 183 – 214 .
   Google Scholar
• Lions , J. L. 1968 . Controle Optimal de Systemes Governes par des Equations aux Derivees Partielles , Paris : Dunod .
   Google Scholar
• Malone , J. B. , Narramore , J. C. and Sankar , L. N. 1991 . Airfoil Design Method Using the Navier-Stokes Equations . J. Aircraft , 28 : 216 – 224 .
   Google Scholar
• Martinex , G. 1979 . Thèse Docteur-Ingénieur , I. N. P. Toulous .
   Google Scholar
• Pironneau , O. 1973 . On Optimum Profiles in Stokes Flow . J. Fluid Mech. , 59 : 117 – 128 .
   Google Scholar
• Pironneau , O. 1974 . On Optimum Design in Fluid Mechanics . J. Fluid Mech. , 64 : 97 – 110 .
   Google Scholar
• Ta Phuoc , Loc . 1980 . Numerical Analysis of Unsteady Secondary Vortices Generated by an Impulsively Started Circular Cylinder . J. Fluid Mechanics , 100 : 111 – 128 .
   Google Scholar
• Tritton , D. J. 1959 . Experiments on the Flow Past a Circular Cylinder at Low Reynolds Numbers . J. Fluid Mechanics , 6 : 547 – 567 .
   Google Scholar
• Tuann , S. Y. and Olson , M. D. 1978 . Computers and Fluid , 6 : 219
   Google Scholar
• Tuck , E. O. Toward the Calculation and Minimization of Stokes Drag Bodies of Arbitrary Shape . Proc. Conf. on Hydraul. and Fluid Mech. Nov. 25–29 1968 , Sydney, Australia. pp. 29 – 32 .
   Google Scholar
• Turkel , E. 1986 . Preconditioned Methods for Solving the Incompressible and Low Speed Compressible Equations . NASA ICASE Report 86–14 ,
   Google Scholar
• Watson , S. R. 1971 . J. Inst. Math. Applics. , 7 : 367 – 376 .
   Google Scholar