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‘Mathematical programming methods for structural optimization’, Struct. Opt. Symp. (Ed. L. A. Schmit), ASME Winter Annual Meeting
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27
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‘Automated structural design with Aeroelastic constraints: a review and assessment of the state of the art’, Struct. Opt. Symp. (Ed. L. A. Schmit), ASME Winter Annual Meeting
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Stroud, W.J.1
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28
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‘Structural optimization via optimal control techniques: a review’, Struct. Opt. Symp. (Ed. L. A. Schmit), ASME Winter Annual Meeting
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‘Structural index methods in optimum design’, Struct. Opt. Symp. (Ed. L. A. Schmit), ASME Winter Annual Meeting
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‘Structural synthesis from abstract concept to practrical tool—synopsis’, Proc. AIAA/ASME 18th Struct., Structural Dynamics and Materials Conf., San Diego, California
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‘Applications of structural optimization for strength and aeroelastic design requirements’, Paper presented at the 45th AGARD Struct. and Materials Panel Meeting, Voss, Norway, AGARD Report No. 664
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AGARD Second Symp. Struct. Opt., AGARD‐CP‐123
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Proc. IUTAM Symp.
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(1977)
ASME Energy Technology Conf. and Exhibitin
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40
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‘Use of optimality criteria methods for large scale systems’, AGARD Lecture Series No. 70, Struct. Opt.
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Optimum design of structures subjected to dynamic loads
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UCLA, School of Engineering and Applied Science
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UCLA‐ENG‐7451
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Cassis, J.H.1
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48
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‘A multilevel approach in optimum design of structures including buckling constraints’, Ph. D. Thesis, University of California, Los Angeles
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(1976)
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Ramanathan, R.K.1
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52
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‘Conmin—a Fortran program for constrained function minimization: user's manual’, NASA TM X‐62
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57
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‘Shape optimization of a load carrying shear plate’, ASME Engng Technology Conf., Houston, Texas (see Reference 38).
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(1977)
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Chun, Y.W.1
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62
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‘Untersuchung and Weiterentwicklung Einiger Verfahren Zur Optimalen Dimensionierung Von Tragwerken’, Instut für Statik and Dynamik Der Luft‐und‐Raumfahrt‐Konstructionen, University of Stuttgart, Report No. BUFT‐RVII‐TU‐3/72B
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Mlejnek, H.P.1
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64
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‘The impact of automated structural optimization on actual design’, AIAA Ppaer No. 73–361
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(1971)
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Tocher, J.L.1
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65
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‘Optimization of structures undergoing harmonic or stochastic excitation’, Ph. D. Dissertation, Department of Aeronautics and Astronautics, Stanford University (also NASA CR‐142, 936).
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(1975)
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Johnson, E.H.1
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69
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‘Automated structural synthesis using a reduced numer of design coordinates’, AIAA Preprint, AIAA/ASME/SAE 14th Struct., Structural Dynamics, and Materials Conf., Williamsburg, Virginia
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(1973)
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Pickett, R.M.1
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71
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84987045571
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‘An efficient approach to the minimum weight design of deffection limited structures’, AFFDL‐TM‐70–4–FDTR
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74
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‘Application of optimality criteria approaches to automated design of large practical structures’, Second Symp. Struct. Opt., AGARD‐CP‐123, Milan, Italy
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(1973)
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Venkayya, V.B.1
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76
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‘Optimum design of composite structures with stress and deflection constraints’, AIAA Paper No. 75–141, represented at AIAA 13th Aerospace Science Meeting, Pasadena, California
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Khot, N.S.1
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78
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‘Experience with minimum weight design of structures using optimality criteria methods’, 2nd Int. Conf. Vehicle Struct. Mech., Southfield, Michigan
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Khot, N.S.1
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79
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‘Comparisons of optimality criteria alogorithms for minimum weight design of structures’, AIAA/ASME 19th SDM Conf., Bethesda, Maryland
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Khot, N.S.1
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80
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‘Optimal structural design’, AFFDL‐TR‐70–165, Air Force Flight Dynamics Laboratory, Wright‐Patterson A. F. B., Ohio
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81
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‘Minimum weight design of structures via optimality criteria’, NASA TN D‐7115
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83
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84
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‘Three contributions to minimum weight structural optimization with dynamic and aeroelastic constraints’, Stanford University, SUDAAR Report No. 501
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85
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(1976)
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88
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‘A rapid optimization procedure for structures subjected to multiple constraints’, Paper No. 77–374, AIAA/ASME/SAE 18th Struct., Structural Dynamics and Materials Conf., San Diego, California
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(1977)
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Austin, F.1
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89
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‘Optimization of aircraft structures with multiple stiffness requirements’, Second Symp. Struct. Opt., AGARD‐CP‐123, Milan, Italy
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(1973)
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Taig, I.C.1
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90
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‘Computer design of antenna reflectors’, AIAA Paper No. 73–351, Presented at the AIAA/ASME/SAE 14th Struct., Structural Dynamics and Materials Conf., Williamsburgh, VA
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(1973)
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Levy, R.1
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92
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‘Application of optimality criteria in structural synthesis’, UCLA‐ENG‐7446
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(1974)
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Terai, K.1
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93
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‘Generalized optimality criteria for structural design’, thesis presented to the University of Toronto, in, in partial fulfillment of the requirements for the degree of Doctor of Philosophy.
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(1977)
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Tabak, E.I.1
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95
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‘A mixed method in structural optimization’, ASME Energy Technology Conf., Houston, Texas (see Reference 38).
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102
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106
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‘A new approach to optimal design of elastic structures’, Division of Engineering, Brown University, Providence, R. I.
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(1973)
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Nagtegaal, J.C.1
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108
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‘Optimal structural design for given deflection under periodic loading’, 8334–15‐E, 1971, AROD, U. S. Army Research Office, Durham, North Carolina.
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AIAA Journal
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‘On the minimum mass layout of trusses’, AGARD CP‐36, Symp. Struct. Opt., Istanbul, October
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Pederson, P.1
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121
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(1973)
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‘Optimum structural design for simultaneous multicomponent static and dynamic inputs’, Paper presented at ASME Energy Technology Conf., Houston, Texas. (See Reference 38.)
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Cheng, F.Y.1
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144
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‘Foundations of aeroelastic optimization and some applications to continuous systems’, SUDAAR 390, Department of Aeronautics and Astronautics, Stanford Univ.
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(1970)
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Armand, J.P.1
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145
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‘Weight minimization of structures for fixed flutter speed via an optimality criterion’, Proc. AIAA/ASME/SAE 16th Struct., Structural Dynamics and Materials Conf., Denver, Colorado
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(1975)
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148
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‘Aeroelastic tailoring of advanced composite lifting surfaces in preliminary design’, Proc. AIAA/ASME/SAE 17th Struct., Structural Dynamics and Materials Conf., Valley Forge, Pennsylvania
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(1976)
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Austin, F.1
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151
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‘An application of control theory methods to the optimization of structures having dynamic or aeroelastic constraints’, SUDAAR 412, Department of Aeronautics and Astronautics, Stanford Univ.
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(1970)
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154
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‘Automated procedure for design of wing structures to satisfy strength and flutter requirements’, NASA TN D‐7262
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(1973)
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Haftka, R.T.1
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155
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‘Composite wing design for aeroelastic requirements’, Proc. Conf. Fibrous Composites in Flight Vehicle Design, AFFDL‐TR‐72‐130, Dayton, Ohio
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(1972)
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157
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‘Aeroelastic tailoring of composite materials to improve performance’, Proc. AIAA/ASME/SAE 17th Struct., Structural Dynamics and Materials Conf., Valley Forge, Pennsylvania
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158
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‘Application of a general method for flutter optimization’, Second symp. Struct. Opt., AGARD‐CP‐123, Milan, Italy
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(1973)
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Taylor, R.F.1
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159
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‘Optimal Aeroelastic design of an oblique wing structure’, AIAA/ASME/SAE 15th SDM Conf., Las Vegas, Nevada
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(1974)
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Gwin, L.B.1
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160
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‘An efficient structural resizing procedure for meeting static aeroelastic design objectives’, AIAA/ASME 19th SDM Conf., Bethesda, Md.
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(1978)
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Lerner, E.1
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168
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‘Evaluation of automated economical design methods for multistory steel frameworks’, Ph. D. thesis, University of California, Davis
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(1972)
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169
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84987007770
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‘Optimum design of frames using linear programming techniques’, thesis presented to Clarkson College of Technology in partial fulfillment of the requirements for the degree of Master of Science
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(1976)
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Briggs, W.J.1
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171
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‘Inclusion of explicit thermal requirements in the optimum design of structures’, NASA TM X‐74017
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The behavior of the fully‐stressed design of structures and its relationship to minimum weight design
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AIAA Journal
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178
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‘Fully stressed dynamically loaded structures’, ASME Publication 74‐WA/DE‐19, ASME Winter Annual Meeting
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‘Convergence and substructuring in fully‐stressed designing’, AGARD CP‐36, Symp. Struct. Opt., Istanhul
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‘On the weight and design of a redundant truss’, ARL‐62–338
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‘The optimization of statically indeterminate structures by means of approximate geometric programming’, AGARD Conf. Proc. No. 123
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‘Applications of the theory of optimal control of distributed‐parameter systems to structural optimization’, CR‐2044, NASA
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(1972)
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Armand, J.L.1
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‘Optimal design of bending elements’, ASME Energy Technology Conf., Houston, Texas (see Reference 38).
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Minimum‐mass design of a plate‐like structure for specified fundamental frequency
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‘An automated design procedure for the design of complex structures’, Ph. D. Thesis, University of California, Berkeley
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‘Application of a gradient projection technique to minimum‐weight design of lifting surfaces with aeroelastic and static constraints’, The Texas Institute for Computational Mechanics, TICOM Report 74–3
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(1974)
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Erbug, I.O.1
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