메뉴 건너뛰기




Volumn 1, Issue , 2007, Pages 138-171

Development of generic CFD-based aerodynamic optimisation tools for helicopter rotor blades

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; HELICOPTER ROTORS; PARAMETERIZATION; RADIAL BASIS FUNCTION NETWORKS; SHAPE OPTIMIZATION; THREE DIMENSIONAL;

EID: 35648977552     PISSN: 10485953     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-3809     Document Type: Conference Paper
Times cited : (35)

References (67)
  • 1
    • 85081479065 scopus 로고    scopus 로고
    • Radial Basis Functions for Unified CFD-CSD Interpolation and Mesh Motion in Aeroelastic simulation
    • Miami, June
    • Kendall, T.C.S. and Allen, C.B. "Radial Basis Functions for Unified CFD-CSD Interpolation and Mesh Motion in Aeroelastic simulation", 25th AIAA Applied Aerodynamics Conference, Miami, June 2007.
    • (2007) 25th AIAA Applied Aerodynamics Conference
    • Kendall, T.C.S.1    Allen, C.B.2
  • 2
    • 35648947800 scopus 로고    scopus 로고
    • Towards Automatic Structured Multiblock Mesh Generation using Robust Transfinite Interpolation
    • Miami, June
    • Allen, C.B., "Towards Automatic Structured Multiblock Mesh Generation using Robust Transfinite Interpolation", 25th AIAA CFD Conference, Miami, June 2007.
    • (2007) 25th AIAA CFD Conference
    • Allen, C.B.1
  • 3
    • 85081481652 scopus 로고    scopus 로고
    • Morris, A., Allen, C.B. and Rendall, T.C.S. Aerodynamic Optimisation using Domain Element Parameterisation with Deformation by Radial Basis Functions: Extension to 3D, submitted to the 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Jan 2008.
    • Morris, A., Allen, C.B. and Rendall, T.C.S. "Aerodynamic Optimisation using Domain Element Parameterisation with Deformation by Radial Basis Functions: Extension to 3D", submitted to the 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Jan 2008.
  • 4
    • 0037473255 scopus 로고    scopus 로고
    • Convergence of Steady and Unsteady Formulations for Inviscid Hovering Rotor Solutions
    • Allen, C.B. "Convergence of Steady and Unsteady Formulations for Inviscid Hovering Rotor Solutions" International Journal for Numerical Methods in Fluids 2003; 41:931-949
    • (2003) International Journal for Numerical Methods in Fluids , vol.41 , pp. 931-949
    • Allen, C.B.1
  • 5
    • 3242674469 scopus 로고    scopus 로고
    • An Unsteady Multiblock Multigrid Scheme for Lifting Forward Flight Rotor Simulation
    • DOI 10.2/fld.711
    • Allen, C.B. "An Unsteady Multiblock Multigrid Scheme for Lifting Forward Flight Rotor Simulation" International Journal for Numerical Methods in Fluids, 2004, 45;973-984 (DOI 10.2/fld.711)
    • (2004) International Journal for Numerical Methods in Fluids , vol.45 , pp. 973-984
    • Allen, C.B.1
  • 7
    • 0032739634 scopus 로고    scopus 로고
    • Status and future of geometry Modeling and Grid Generation for Design and Optimisation
    • Samareh J.A. "Status and future of geometry Modeling and Grid Generation for Design and Optimisation", Journal of Aircraft, VOl 36, No1, 1999, pp97-104
    • (1999) Journal of Aircraft, VOl , vol.36 , Issue.NO1 , pp. 97-104
    • Samareh, J.A.1
  • 8
    • 0035336348 scopus 로고    scopus 로고
    • Survey of Shape parameterization techniques for High-Fidelity Multidisciplinary Shape Optimisation
    • May
    • Samareh J.A. "Survey of Shape parameterization techniques for High-Fidelity Multidisciplinary Shape Optimisation" AIAA Journal, Vol 39, No5, May 2001, pp 877-884
    • (2001) AIAA Journal , vol.39 , Issue.NO5 , pp. 877-884
    • Samareh, J.A.1
  • 9
    • 0015613677 scopus 로고
    • Automated Structural Synthesis Using a Reduced Number of Design Coordinates
    • Pickett, R.M., Rubinstein, M.F. and Nelson, R.B. "Automated Structural Synthesis Using a Reduced Number of Design Coordinates" AIAA Journal, VOl 11, No 4, 1973 pp 494-498
    • (1973) AIAA Journal, VOl , vol.11 , Issue.4 , pp. 494-498
    • Pickett, R.M.1    Rubinstein, M.F.2    Nelson, R.B.3
  • 13
    • 0029410083 scopus 로고
    • Efficient Parameterization of Generic Aircraft Geometry
    • Journal of Aircraft, ppl269, 1275
    • Bloor, M.I.G. and Wilson, M.J. "Efficient Parameterization of Generic Aircraft Geometry", Journal of Aircraft, Vol 32, No 6, 1995, ppl269, 1275.
    • (1995) , vol.32 , Issue.6
    • Bloor, M.I.G.1    Wilson, M.J.2
  • 15
    • 85081483016 scopus 로고    scopus 로고
    • J. L. Zhou, A. L. Tits and C. T. Lawrence, User's Guide for FFSQP Version 3.7 : A Fortran Code for Solving Optimization Programs, Possibly Minimax, with General Inequality Constraints and Linear Equality Constraints, Generating Feasible Iterates, Institute for Systems Research, University of Maryland.Technical Report SRC-TR-92-107r5, College Park, MD 20742, 1997.
    • J. L. Zhou, A. L. Tits and C. T. Lawrence, "User's Guide for FFSQP Version 3.7 : A Fortran Code for Solving Optimization Programs, Possibly Minimax, with General Inequality Constraints and Linear Equality Constraints, Generating Feasible Iterates", Institute for Systems Research, University of Maryland.Technical Report SRC-TR-92-107r5, College Park, MD 20742, 1997.
  • 17
    • 19444362308 scopus 로고
    • On Combining Feasibility, Descent and Superlinear Convergence In Inequality Constrained Optimization
    • E. Panier and A. L. Tits, "On Combining Feasibility, Descent and Superlinear Convergence In Inequality Constrained Optimization", Mathematical Programming, Vol. 59(1993), 261-276.
    • (1993) Mathematical Programming , vol.59 , pp. 261-276
    • Panier, E.1    Tits, A.L.2
  • 18
    • 85086054628 scopus 로고    scopus 로고
    • Reuther, J. Jameson, A. Farmer, J. Martinelli, L. and Saunders, D. Aerodynamic Shape Optimization of Complex Aircraft Configurations via an Adjoint Formulation RIACS Technical Report 96.02 January 1996 Presented at the AIAA 34th Aerospace Sciences Meeting and Exhibit, January 1996, AIAA paper 96-0094
    • Reuther, J. Jameson, A. Farmer, J. Martinelli, L. and Saunders, D. " Aerodynamic Shape Optimization of Complex Aircraft Configurations via an Adjoint Formulation" RIACS Technical Report 96.02 January 1996 Presented at the AIAA 34th Aerospace Sciences Meeting and Exhibit, January 1996, AIAA paper 96-0094
  • 20
    • 34147134975 scopus 로고    scopus 로고
    • Parallel adjoint-based optimisation of a blended wing body aircraft with shck control bumps
    • March
    • W.S. Wong, A. Le Moigne and N. Qin, "Parallel adjoint-based optimisation of a blended wing body aircraft with shck control bumps", The Aeronautical Journal, Volume 111, Number 1117, March 2007
    • (2007) The Aeronautical Journal , vol.111 , Issue.1117
    • Wong, W.S.1    Le Moigne, A.2    Qin, N.3
  • 21
    • 18244381784 scopus 로고    scopus 로고
    • Spanwise lift distribution for blended wing body aircraft
    • N. Qin, A. Vavalle and A. Le Moigne, "Spanwise lift distribution for blended wing body aircraft", J of Aircraft, Vol.42, No.2, 2005, PP356-365.
    • (2005) J of Aircraft , vol.42 , Issue.2
    • Qin, N.1    Vavalle, A.2    Le Moigne, A.3
  • 25
    • 35648981170 scopus 로고    scopus 로고
    • Mesh deformation using radial basis functions for gradient-based aerodynamic shape optimisation
    • FOI-R-1784-SE, December 2005
    • S.Jakobsson and O.Amoignon "Mesh deformation using radial basis functions for gradient-based aerodynamic shape optimisation" FOI report FOI-R-1784-SE, December 2005
    • FOI report
    • Jakobsson, S.1    Amoignon, O.2
  • 26
    • 0017995820 scopus 로고
    • Wing Design by Numerical Optimization
    • Hicks, R.M. and Henne, P.A. "Wing Design by Numerical Optimization" Journal of Aircraft, 15:407-412, 1978.
    • (1978) Journal of Aircraft , vol.15 , pp. 407-412
    • Hicks, R.M.1    Henne, P.A.2
  • 28
    • 85081485617 scopus 로고    scopus 로고
    • M.Drela A users guide to LINDOP V2.5 MIT Computational Aerospaces Sciences Laboratory, June 1996
    • M.Drela "A users guide to LINDOP V2.5" MIT Computational Aerospaces Sciences Laboratory, June 1996
  • 30
    • 15844409428 scopus 로고    scopus 로고
    • A. Le Pape, A Beaumier, P. Numerical Optimisation of Helicopter Rotor Aerodynamic Performance in Hover Aerospace Science and Technology 9 (2005) 191-201
    • A. Le Pape, A Beaumier, P. " Numerical Optimisation of Helicopter Rotor Aerodynamic Performance in Hover" Aerospace Science and Technology 9 (2005) 191-201
  • 32
    • 84888765347 scopus 로고    scopus 로고
    • Robust Aerofoil Optimization to Achieve Consistent Drag Reduction Over a Mach Range NASA/CR-2001-211042
    • no 2001-22
    • Li, W. Huyse, L. Padula, S. "Robust Aerofoil Optimization to Achieve Consistent Drag Reduction Over a Mach Range" NASA/CR-2001-211042. icase report no 2001-22
    • icase report
    • Li, W.1    Huyse, L.2    Padula, S.3
  • 33
    • 51349130598 scopus 로고    scopus 로고
    • Profile Optimization Method for Robust Aerofoil Shape Optimization in Viscous Flows NASA/TM-2003-212408. NASA/CR-2001-211042
    • no 2001-22
    • Li, W. Huyse, L. Padula, S. "Profile Optimization Method for Robust Aerofoil Shape Optimization in Viscous Flows" NASA/TM-2003-212408. NASA/CR-2001-211042. icase report no 2001-22
    • icase report
    • Li, W.1    Huyse, L.2    Padula, S.3
  • 38
    • 0003424880 scopus 로고    scopus 로고
    • Aerodynamic Shape Optimization Using Control Theory
    • NASA-CR-201064, 1996
    • Reuther, J "Aerodynamic Shape Optimization Using Control Theory", NASA Technical report NASA-CR-201064, 1996
    • NASA Technical report
    • Reuther, J.1
  • 39
    • 0002975311 scopus 로고
    • Optimum Aerodynamic Design Using Control Theory
    • Jameson, A. "Optimum Aerodynamic Design Using Control Theory" Computational Fluid Dynamics Review, 1995, pp. 495-528.
    • (1995) Computational Fluid Dynamics Review , pp. 495-528
    • Jameson, A.1
  • 40
    • 85081484455 scopus 로고    scopus 로고
    • Comparison of Three Geometric Representations of Aerofoils for Aerodynamic Design for Optimization
    • AIAA 2003-4095, June 23-26, Orlando Florida
    • Wu, H-Y. Yang, S. Liu, F. "Comparison of Three Geometric Representations of Aerofoils for Aerodynamic Design for Optimization" AIAA 2003-4095, 16th computational fluid dynamics conference, June 23-26, Orlando Florida.
    • 16th computational fluid dynamics conference
    • Wu, H.-Y.1    Yang, S.2    Liu, F.3
  • 42
    • 0026944950 scopus 로고
    • Aerodynamic Shape design and Optimization: Status and trends
    • Nov-Dec
    • Dulikravich, S. G. "Aerodynamic Shape design and Optimization: Status and trends" Journal of Aircraft, Vol 29, No.6. Nov-Dec 1992
    • (1992) Journal of Aircraft , vol.29 , Issue.6
    • Dulikravich, S.G.1
  • 43
    • 0032739432 scopus 로고    scopus 로고
    • Recent Applications of Design Optimization to Rotorcraft - A Survey
    • Celi, R. "Recent Applications of Design Optimization to Rotorcraft - A Survey" J. Aircraft 36 (1) (1999)
    • (1999) J. Aircraft , vol.36 , Issue.1
    • Celi, R.1
  • 45
    • 0038628504 scopus 로고
    • Numerical Algorithms Based on the Theory of Complex Variables
    • Thomas Book Co, Washington, D.C
    • Lyness, J.N., "Numerical Algorithms Based on the Theory of Complex Variables", Proc. ACM 22nd Nat. Conf. Thomas Book Co., Washington, D.C., 1967, pp. 124-134.
    • (1967) Proc. ACM 22nd Nat. Conf , pp. 124-134
    • Lyness, J.N.1
  • 46
  • 48
    • 20544476549 scopus 로고
    • Aerodynamic design via control theory
    • Jameson, A. "Aerodynamic design via control theory" J Sci Comput 1988;3:233-60
    • (1988) J Sci Comput , vol.3 , pp. 233-260
    • Jameson, A.1
  • 49
    • 3342993306 scopus 로고    scopus 로고
    • A discrete Navier-Stokes adjoint method for aerodynamic optimisation of Blended-Wing-Body configurations
    • Phd Thesis, Cranfield University College of Aeronautics
    • Le Moigne, A. "A discrete Navier-Stokes adjoint method for aerodynamic optimisation of Blended-Wing-Body configurations" Phd Thesis, Cranfield University College of Aeronautics
    • Le Moigne, A.1
  • 50
    • 0035578487 scopus 로고    scopus 로고
    • Multivariate Interpolation for Fluid-Structure-Interpolation Problems using Radial Basis Functions
    • May-June
    • Beckert, A. and Wendland, H. "Multivariate Interpolation for Fluid-Structure-Interpolation Problems using Radial Basis Functions", Aerospace Science and Technology, 5:125-134, May-June 2001
    • (2001) Aerospace Science and Technology , vol.5 , pp. 125-134
    • Beckert, A.1    Wendland, H.2
  • 51
    • 3042799255 scopus 로고    scopus 로고
    • Cambridge University Press, 1st edition
    • Buhmann, H. "Radial Basis Functions", Cambridge University Press, 1st edition, 2005
    • (2005) Radial Basis Functions
    • Buhmann, H.1
  • 53
    • 85081490050 scopus 로고    scopus 로고
    • Wells, V. L. Han, A. Y. and Crossley, W. A. Acoustic Design of Rotor Blades Using a Genetic Algorithm Aerodynamics and Aeroacoustics of Rotorcraft, AGARD CP-552, Aug 1995, pp. 35.135.10
    • Wells, V. L. Han, A. Y. and Crossley, W. A. "Acoustic Design of Rotor Blades Using a Genetic Algorithm" Aerodynamics and Aeroacoustics of Rotorcraft, AGARD CP-552, Aug 1995, pp. 35.135.10
  • 57
    • 0030247818 scopus 로고    scopus 로고
    • Parallel Genetic Algorithm Implementation in Multidisciplinary Rotor Blade Design
    • Sep-Oct
    • Lee, J. and Hajela, P. "Parallel Genetic Algorithm Implementation in Multidisciplinary Rotor Blade Design" Journal of Aircraft, Vol. 33, No. 5, Sep-Oct 1996, pp. 962-969
    • (1996) Journal of Aircraft , vol.33 , Issue.5 , pp. 962-969
    • Lee, J.1    Hajela, P.2
  • 58
    • 85081487922 scopus 로고    scopus 로고
    • Schittkowski, K Test examples for nonlinear programming codes: Supplement, Report, Institute for Information technology, University of Stuttgart, 1984
    • Schittkowski, K "Test examples for nonlinear programming codes: Supplement", Report, Institute for Information technology, University of Stuttgart, 1984
  • 62
    • 0343228755 scopus 로고    scopus 로고
    • Elements of Computational Fluid Dynamics on Block Structured Grids Using Implicit Solvers
    • Richards, B.E., Badcock, K.J. and Woodgate, M.A., "Elements of Computational Fluid Dynamics on Block Structured Grids Using Implicit Solvers", Progress in Aerospace Sciences, Vol. 36, 2000, pp351-392.
    • (2000) Progress in Aerospace Sciences , vol.36 , pp. 351-392
    • Richards, B.E.1    Badcock, K.J.2    Woodgate, M.A.3
  • 63
    • 85081484403 scopus 로고    scopus 로고
    • http://www.optimalsolutions.us/
  • 65
    • 34250824189 scopus 로고    scopus 로고
    • A Universal Parametric Geometry Representation Method -CST
    • 8-11 Jan, Reno, Nevada
    • Kulfan, B. M. "A Universal Parametric Geometry Representation Method -CST" 45th AIAA Aerospace Sciences Meeting and Exhibit 8-11 Jan 2007, Reno, Nevada
    • (2007) 45th AIAA Aerospace Sciences Meeting and Exhibit
    • Kulfan, B.M.1
  • 66
    • 0003600635 scopus 로고
    • Aerofoil RAE 2822 - Pressure Distributions, and Boundary Layer and Wake Measurements
    • Experimental Data Base for Computer Program Assessment, AGARD Report AR 138
    • Cook, P.H., M.A. McDonald, M.C.P. Firmin, "Aerofoil RAE 2822 - Pressure Distributions, and Boundary Layer and Wake Measurements", Experimental Data Base for Computer Program Assessment, AGARD Report AR 138, 1979.
    • (1979)
    • Cook, P.H.1    McDonald, M.A.2    Firmin, M.C.P.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.