1–20 von 22 Ergebnissen
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    Integrated aerodynamic/structural design of a sailplane wing

    Grossman, B. / Gurdal, Z. / Haftka, R. T. et al. | NTRS | 1988

    Integrated aerodynamic-structural design of a transport wing

    Grossman, B. / Haftka, R. T. / Sobieszczanski-Sobieski, Jaroslaw et al. | NTRS | 1990

    Integrated aerodynamic-structural-control wing design

    Rais-Rohani, M. / Haftka, R. T. / Grossman, B. et al. | NTRS | 1992

    Variable-complexity aerodynamic-structural design of a high-speed civil transport wing

    Hutchison, M. G. / Huang, X. / Mason, W. H. et al. | NTRS | 1992

    Aerodynamic optimization of an HSCT configuration using variable-complexity modeling

    Hutchison, M. G. / Mason, W. H. / Grossman, B. et al. | NTRS | 1993

    Sensitivity algorithms for an inverse design problem involving a shock wave

    Narducci, R. / Grossman, B. / Haftka, R. | AIAA | 1994

      Sensitivity Algorithms for an Inverse Design Problem Involving a Shock Wave

      Narducci, R. / Grossman, B. / Haftka, R. T. et al. | British Library Conference Proceedings | 1994

    Variable-complexity aerodynamic optimization of a high-speed civil transport wing

    Hutchison, M. G. / Unger, E. R. / Mason, W. H. et al. | AIAA | 1994

    Comparison of Statistical Weight Equations with Structural Optimization for Supersonic Transport Wings

    Huang, X. / Haftka, R. / Grossman, B. et al. | British Library Conference Proceedings | 1994

    Variable-Complexity Interlacing of Weight Equation and Structural Optimization for the Design of the High-Speed Civil Transport

    Huang, X. / Dudley, J. / Haftka, R. et al. | British Library Conference Proceedings | 1994

    Multifidelity Response Surface Model for HSCT Wing Bending Material Weight

    Balabanov, V. / Haftka, R. / Grossman, B. et al. | British Library Conference Proceedings | 1998

    HSCT Configuration Design Space Exploration Using Aerodynamic Response Surface Approximations

    Baker, C. / Grossman, B. / Haftka, R. et al. | British Library Conference Proceedings | 1998

    Multidisciplinary Design Optimization of a Transonic Commercial Transport with a Strut-Braced Wing

    Ko, A. / Naghshineh-Pour, A. / Grossman, B. et al. | SAE Technical Papers | 1999

    The role of constraints in the MDO of a cantilever and strut-braced wing transonic commercial transport aircraft

    Ko, A. / Grossman, B. / Mason, W. et al. | AIAA | 2000

      The Role of Constraints in the MDO of a Cantilever and Strut-Braced Wing Transonic Commercial Transport Aircraft

      Ko, A. / Grossman, B. / Mason, W. H. et al. | British Library Conference Proceedings | 2000

    STUDY OF A GLOBAL DESIGN SPACE EXPLORATION METHOD FOR AEROSPACE VEHICLES

    Baker, C. A. / Watson, L. T. / Grossman, B. et al. | British Library Conference Proceedings | 2000

    Multidisciplinary Design Optimization of a Strut-Braced Wing Transonic Transport

    Gundlach, J. F. / Tetrault, P.-A. / Gern, F. et al. | British Library Conference Proceedings | 2000

    Detection and Correction of Poorly Converged Optimizations by Iteratively Reweighted Least Squares

    Grossman, B. / Haftka, R. / Kim, H. et al. | British Library Conference Proceedings | 2000

    AIAA-2002-5576 Estimating Optimization Error Statistics via Optimization Runs from Multiple Starting Points

    Kim, H. / Papila, M. / Haftka, R. et al. | British Library Conference Proceedings | 2002

    AIAA-2003-6732 MDO of a Blended-Wing-Body Transport Aircraft with Distributed Propulsion

    Ko, A. / Mason, W. / Grossman, B. et al. | British Library Conference Proceedings | 2003