-
1
-
-
0017995820
-
Wing design by numerical optimization
-
Hicks RM, Henne PA. Wing design by numerical optimization. Journal of Aircraft 1978; 15:407-412.
-
(1978)
Journal of Aircraft
, vol.15
, pp. 407-412
-
-
Hicks, R.M.1
Henne, P.A.2
-
2
-
-
0345341497
-
An assessment of aerofoil design by numerical optimization
-
Ames Research Center, Moffett Field, CA, July
-
Hicks RM, Murman EM, Vanderplaats GN. An assessment of aerofoil design by numerical optimization. NASA TMX-3092, Ames Research Center, Moffett Field, CA, July 1974.
-
(1974)
NASA TMX-3092
-
-
Hicks, R.M.1
Murman, E.M.2
Vanderplaats, G.N.3
-
3
-
-
0005316912
-
NASA/CR-2001-211042, Icase Report 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.
-
-
-
Li, W.1
Huyse, L.2
Padula, S.3
-
4
-
-
73949095326
-
NASA/TM-2003-212408, NASA/ CR-2001-211042, Icase Report 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.
-
-
-
Li, W.1
Huyse, L.2
Padula, S.3
-
5
-
-
34147134975
-
Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps
-
Wong WS, Le Moigne A, Qin N. Parallel adjoint-based optimisation of a blended wing body aircraft with shock control bumps. The Aeronautical Journal 2007; 111(1117):165-174.
-
(2007)
The Aeronautical Journal
, vol.111
, Issue.1117
, pp. 165-174
-
-
Wong, W.S.1
Le Moigne, A.2
Qin, N.3
-
6
-
-
18244381784
-
Spanwise lift distribution for blended wing body aircraft
-
Qin N, Vavalle A, Le Moigne A. Spanwise lift distribution for blended wing body aircraft. Journal of Aircraft 2005; 42(2):356-365.
-
(2005)
Journal of Aircraft
, vol.42
, Issue.2
, pp. 356-365
-
-
Qin, N.1
Vavalle, A.2
Le Moigne, A.3
-
7
-
-
35648931896
-
Validation and optimisation of 3D bumps for transonic wing drag reduction
-
Bremen, Germany, June
-
Qin N, Wong WS, LeMoigne A, Sellars N. Validation and optimisation of 3D bumps for transonic wing drag reduction. CEAS/Ketnet Conference on Key Aerodynamic Technologies, Bremen, Germany, June 2005.
-
(2005)
CEAS/Ketnet Conference on Key Aerodynamic Technologies
-
-
Qin, N.1
Wong, W.S.2
LeMoigne, A.3
Sellars, N.4
-
8
-
-
84879023904
-
Aerodynamic studies of blended wing body aircraft
-
Atlanta, GA, September
-
Qin N, Vavalle A, Le Moigne A, Laban M, Huckett K, Weinerfelt P. Aerodynamic studies of blended wing body aircraft. The 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization Conference, AIAA-2002-5448, Atlanta, GA, September 2002.
-
(2002)
The 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization Conference, AIAA-2002-5448
-
-
Qin, N.1
Vavalle, A.2
Le Moigne, A.3
Laban, M.4
Huckett, K.5
Weinerfelt, P.6
-
9
-
-
85086054628
-
Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation
-
January
-
Reuther J, Jameson A, Farmer J, Martinelli L, 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, AIAA Paper 96-0094, January 1996.
-
(1996)
RIACS Technical Report 96.02 January 1996 Presented at the AIAA 34th Aerospace Sciences Meeting and Exhibit, AIAA Paper 96-0094
-
-
Reuther, J.1
Jameson, A.2
Farmer, J.3
Martinelli, L.4
Saunders, D.5
-
10
-
-
20344406826
-
Multiobjective optimization using approximation model-based genetic algorithms. Tenth
-
Albany, New York, AIAA, 30 August-1 September
-
Chung HS, Alonso J. Multiobjective optimization using approximation model-based genetic algorithms. Tenth AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Albany, New York, AIAA 2004-4325, 30 August-1 September 2004.
-
(2004)
AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
, vol.4325
-
-
Chung, H.S.1
Alonso, J.2
-
11
-
-
84983185715
-
-
Gumbert CR, Hou G, Newman PA. Simultaneous aerodynamic analysis and design optimization (SAADO) for a 3-D rigid wing. Fourteenth AIAA Computational Fluid Dynamics Conference, Norfolk, VA, AIAA 99-3296, 28 June-1 July 1999.
-
Gumbert CR, Hou G, Newman PA. Simultaneous aerodynamic analysis and design optimization (SAADO) for a 3-D rigid wing. Fourteenth AIAA Computational Fluid Dynamics Conference, Norfolk, VA, AIAA 99-3296, 28 June-1 July 1999.
-
-
-
-
12
-
-
27444434520
-
Simultaneous aerodynamic analysis and design optimization (SAADO) for a 3-D flexible wing
-
Gumbert CR, Hou G, Newman PA. Simultaneous aerodynamic analysis and design optimization (SAADO) for a 3-D flexible wing. AIAA 2001-1107, 2001.
-
(2001)
AIAA
, vol.2001 -1107
-
-
Gumbert, C.R.1
Hou, G.2
Newman, P.A.3
-
13
-
-
15844409428
-
Numerical optimisation of helicopter rotor aerodynamic performance in hover
-
Le Pape A, Beaumier P. Numerical optimisation of helicopter rotor aerodynamic performance in hover. Aerospace Science and Technology 2005; 9:191-201.
-
(2005)
Aerospace Science and Technology
, vol.9
, pp. 191-201
-
-
Le Pape, A.1
Beaumier, P.2
-
14
-
-
61849112818
-
-
Le Pape A. Numerical aerodynamic optimization of helicopter rotors. ERF, Florence, September 2005.
-
Le Pape A. Numerical aerodynamic optimization of helicopter rotors. ERF, Florence, September 2005.
-
-
-
-
15
-
-
0343228755
-
Elements of computational fluid dynamics on block structured grids using implicit solvers
-
Richards BE, Badcock KJ, Woodgate MA. Elements of computational fluid dynamics on block structured grids using implicit solvers. Progress in Aerospace Sciences 2000; 36:351-392.
-
(2000)
Progress in Aerospace Sciences
, vol.36
, pp. 351-392
-
-
Richards, B.E.1
Badcock, K.J.2
Woodgate, M.A.3
-
16
-
-
42949096173
-
Towards automatic structured multiblock mesh generation using improved transfinite interpolation
-
DOI: 10.1002/nme.2170
-
Allen CB. Towards automatic structured multiblock mesh generation using improved transfinite interpolation. International Journal for Numerical Methods in Engineering 2008; DOI: 10.1002/nme.2170.
-
(2008)
International Journal for Numerical Methods in Engineering
-
-
Allen, C.B.1
-
17
-
-
0029410083
-
Efficient parameterization of generic aircraft geometry
-
Bloor MIG, Wilson MJ. Efficient parameterization of generic aircraft geometry. Journal of Aircraft 1995; 32(6):1269-1275.
-
(1995)
Journal of Aircraft
, vol.32
, Issue.6
, pp. 1269-1275
-
-
Bloor, M.I.G.1
Wilson, M.J.2
-
18
-
-
84983196986
-
Rapid airplane parametric input design (RAPID)
-
AIAA: Washington, DC
-
Smith RE, Bloor MIG, Wilson MJ, Thomas AT. Rapid airplane parametric input design (RAPID). Proceedings of 12th AIAA Computational Fluid Dynamics Conference. AIAA: Washington, DC, 1995; 452-462.
-
(1995)
Proceedings of 12th AIAA Computational Fluid Dynamics Conference
, pp. 452-462
-
-
Smith, R.E.1
Bloor, M.I.G.2
Wilson, M.J.3
Thomas, A.T.4
-
20
-
-
33846559928
-
-
Kulfan BM, Bussoletti JE. Fundamental parametric geometry representations for aircraft component shapes. Eleventh AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Renaissance Portsmouth, VA, AIAA-2006-6948, 6-8 September 2006.
-
Kulfan BM, Bussoletti JE. Fundamental parametric geometry representations for aircraft component shapes. Eleventh AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Renaissance Portsmouth, VA, AIAA-2006-6948, 6-8 September 2006.
-
-
-
-
22
-
-
0344478840
-
Inexactness and global convergence in design optimization
-
Panama City, FL, AIAA Paper 94-4286, September
-
DYoung DP, Huffman WP, Melvin RG, Bieterman MB, Hilmes CL, Johnson FT. Inexactness and global convergence in design optimization. Fifth AIAA/ USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization, Panama City, FL, AIAA Paper 94-4286, September 1994.
-
(1994)
Fifth AIAA/ USAF/NASA/ISSMO Symposium on Multidisciplinary Analysis and Optimization
-
-
DYoung, D.P.1
Huffman, W.P.2
Melvin, R.G.3
Bieterman, M.B.4
Hilmes, C.L.5
Johnson, F.T.6
-
24
-
-
0003424880
-
Aerodynamic shape optimization using control theory
-
NASA-CR-201064
-
Reuther J. Aerodynamic shape optimization using control theory. NASA Technical Report NASA-CR-201064, 1996.
-
(1996)
NASA Technical Report
-
-
Reuther, J.1
-
25
-
-
61849133942
-
-
Sobieczky H. Parametric Airfoils and Wings. Notes on Numerical Fluid Mechanics, 68. Vieweg Verlag, 1998; 71-88.
-
Sobieczky H. Parametric Airfoils and Wings. Notes on Numerical Fluid Mechanics, vol. 68. Vieweg Verlag, 1998; 71-88.
-
-
-
-
26
-
-
84897722354
-
-
Wu H-Y, Yang S, Liu F. Comparison of three geometric representations of aerofoils for aerodynamic design for optimization. Sixteenth Computational Fluid Dynamics Conference, Orlando FL, AIAA 2003-4095, 23-26 June 2003.
-
Wu H-Y, Yang S, Liu F. Comparison of three geometric representations of aerofoils for aerodynamic design for optimization. Sixteenth Computational Fluid Dynamics Conference, Orlando FL, AIAA 2003-4095, 23-26 June 2003.
-
-
-
-
27
-
-
35648980955
-
Survey of shape parameterization techniques and its effect on three dimensional aerodynamic shape optimization
-
Miami, FL, 25-28 June
-
Nadarajah S, Castonguay P, Mousavi A. Survey of shape parameterization techniques and its effect on three dimensional aerodynamic shape optimization. Eighteenth AIAA Computational Fluid Dynamics Conference, Miami, FL, AIAA-2007-3837, 25-28 June 2007.
-
(2007)
Eighteenth AIAA Computational Fluid Dynamics Conference
, vol.AIAA-2007-3837
-
-
Nadarajah, S.1
Castonguay, P.2
Mousavi, A.3
-
28
-
-
20544476549
-
Aerodynamic design via control theory
-
Jameson A. Aerodynamic design via control theory. Journal of Scientific Computing 1988; 3:233-260.
-
(1988)
Journal of Scientific Computing
, vol.3
, pp. 233-260
-
-
Jameson, A.1
-
30
-
-
0015613677
-
Automated structural synthesis using a reduced number of design coordinates
-
Pickett RM, Rubinstein MF, Nelson RB. Automated structural synthesis using a reduced number of design coordinates. AIAA Journal 1973; 11(4):494-498.
-
(1973)
AIAA Journal
, vol.11
, Issue.4
, pp. 494-498
-
-
Pickett, R.M.1
Rubinstein, M.F.2
Nelson, R.B.3
-
32
-
-
61849159355
-
-
http://www.optimalsolutions.us/.
-
-
-
-
33
-
-
0002975311
-
Optimum aerodynamic design using control theory
-
Hafez M, Oshima K eds, Wiley: U.K
-
Jameson A. Optimum aerodynamic design using control theory. In Computational Fluid Dynamics Review, Hafez M, Oshima K (eds). Wiley: U.K., 1995; 495-528.
-
(1995)
Computational Fluid Dynamics Review
, pp. 495-528
-
-
Jameson, A.1
-
34
-
-
61849114691
-
-
Drela M. A Users Guide to LINDOP V2.5. MIT Computational Aerospaces Sciences Laboratory, 1996.
-
Drela M. A Users Guide to LINDOP V2.5. MIT Computational Aerospaces Sciences Laboratory, 1996.
-
-
-
-
35
-
-
61849100531
-
-
Drela M. A Users Guide to MSES 2.95. MIT Computational Aerospaces Sciences Laboratory, 1996.
-
Drela M. A Users Guide to MSES 2.95. MIT Computational Aerospaces Sciences Laboratory, 1996.
-
-
-
-
36
-
-
0032739634
-
Status and future of geometry modeling and grid generation for design and optimisation
-
Samareh JA. Status and future of geometry modeling and grid generation for design and optimisation. Journal of Aircraft 1999; 36(1):97-104.
-
(1999)
Journal of Aircraft
, vol.36
, Issue.1
, pp. 97-104
-
-
Samareh, J.A.1
-
37
-
-
0035336348
-
Survey of shape parameterization techniques for high-fidelity multidisciplinary shape optimisation
-
Samareh JA. Survey of shape parameterization techniques for high-fidelity multidisciplinary shape optimisation. AIAA Journal 2001; 39(5):877-884.
-
(2001)
AIAA Journal
, vol.39
, Issue.5
, pp. 877-884
-
-
Samareh, J.A.1
-
39
-
-
19444362308
-
On combining feasibility, descent and superlinear convergence in inequality constrained optimization
-
Panier E, Tits AL. On combining feasibility, descent and superlinear convergence in inequality constrained optimization. Mathematical Programming 1993; 59:261-276.
-
(1993)
Mathematical Programming
, vol.59
, pp. 261-276
-
-
Panier, E.1
Tits, A.L.2
-
44
-
-
61849086841
-
-
Polak1 E, Tits AL. System Modeling and Optimization. Lecture Notes in Control and Information Sciences, 38/1982. Springer: Berlin, Heidelberg, 1982.
-
Polak1 E, Tits AL. System Modeling and Optimization. Lecture Notes in Control and Information Sciences, vol. 38/1982. Springer: Berlin, Heidelberg, 1982.
-
-
-
-
45
-
-
61849126858
-
Test examples for nonlinear programming codes: Supplement
-
Report, Institute for Information Technology, University of Stuttgart
-
Schittkowski K. Test examples for nonlinear programming codes: supplement. Report, Institute for Information Technology, University of Stuttgart, 1984.
-
(1984)
-
-
Schittkowski, K.1
-
46
-
-
0003997741
-
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
-
Technical Report SRC-TR-92-107r5, Institute for Systems Research, University of Maryland, MD
-
Zhou JL, Tits AL, Lawrence CT. 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. Technical Report SRC-TR-92-107r5, Institute for Systems Research, University of Maryland, MD, 1997.
-
(1997)
-
-
Zhou, J.L.1
Tits, A.L.2
Lawrence, C.T.3
-
48
-
-
35648977552
-
Development of Generic CFD-based aerodynamic optimisation tools for helicopter rotor blades
-
Miami, June
-
Morris A, Allen CB, Rendall TCS. Development of Generic CFD-based aerodynamic optimisation tools for helicopter rotor blades. Twenty-fifth AIAA Applied Aerodynamics Conference, Miami, AIAA 2007-3809, June 2007.
-
(2007)
Twenty-fifth AIAA Applied Aerodynamics Conference
, vol.AIAA 2007-3809
-
-
Morris, A.1
Allen, C.B.2
Rendall, T.C.S.3
-
49
-
-
35648981170
-
Mesh deformation using radial basis functions for gradient-based aerodynamic shape optimisation
-
FOI-R-1784-SE, December
-
Jakobsson S, Amoignon O. Mesh deformation using radial basis functions for gradient-based aerodynamic shape optimisation. FOI Report FOI-R-1784-SE, December 2005.
-
(2005)
FOI Report
-
-
Jakobsson, S.1
Amoignon, O.2
-
50
-
-
0035578487
-
Multivariate interpolation for fluid-structure-interpolation problems using radial basis functions
-
Beckert A, Wendland H. Multivariate interpolation for fluid-structure-interpolation problems using radial basis functions. Aerospace Science and Technology 2001; 5:125-134.
-
(2001)
Aerospace Science and Technology
, vol.5
, pp. 125-134
-
-
Beckert, A.1
Wendland, H.2
-
51
-
-
3042799255
-
-
1st edn, Cambridge University Press: Cambridge
-
Buhmann H. Radial Basis Functions (1st edn). Cambridge University Press: Cambridge, 2005.
-
(2005)
Radial Basis Functions
-
-
Buhmann, H.1
-
52
-
-
29744465941
-
-
1st edn, Cambridge University Press: Cambridge
-
Wendland H. Scattered Data Approximation (1st edn). Cambridge University Press: Cambridge, 2005.
-
(2005)
Scattered Data Approximation
-
-
Wendland, H.1
-
54
-
-
0003361172
-
Aerofoil RAE 2822 - pressure distributions, and boundary layer and wake measurements
-
AR, Experimental Data Base for Computer Program Assessment
-
Cook PH, McDonald MA, Firmin MCP. Aerofoil RAE 2822 - pressure distributions, and boundary layer and wake measurements. AGARD Report AR 138, Experimental Data Base for Computer Program Assessment, 1979.
-
(1979)
AGARD Report
, vol.138
-
-
Cook, P.H.1
McDonald, M.A.2
Firmin, M.C.P.3
|