1–20 of 34 hits
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    A modular adjoint approach to aircraft mission analysis and optimization

    Kao, Jason / Hwang, John / Martins, Joaquim R. R. A. et al. | AIAA | 2015

    A Non-Gaussian Gust Model for Aircraft Response Analysis

    W. S. Pi / Chintsun Hwang | AIAA | 1978

    Automatic Evaluation of Multidisciplinary Derivatives Using a Graph-Based Problem Formulation in OpenMDAO

    Gray, Justin S. / Hearn, Tristan A. / Moore, Kenneth T. et al. | AIAA | 2014

    Convective model of hartmann flow

    FAN, L. T. / HWANG, C. L. / HWANG, W. S. | AIAA | 1964

    Current collection model on tether satellite system

    HWANG, K. / WU, S. / STONE, N. et al. | AIAA | 1990

    Development of the Mars Science Laboratory Heatshield Thermal Protection System

    Beck, Robin A. S. / Driver, David M. / Wright, Michael J. et al. | AIAA | 2014

    Implementation of topology optimization using openMDAO

    Chung, Hayoung / Hwang, John T. / Gray, Justin S. et al. | AIAA | 2018

    Kona: A Parallel Optimization Library for Engineering-Design Problems

    Dener, Alp / Meng, Pengfei / Hicken, Jason E. et al. | AIAA | 2016

    Model reduction for hypersonic flows in thermochemical non-equilibrium.

    Joshi, Susmit S. / Hwang, Wontae / Choi, Seongim | AIAA | 2023

    Multidisciplinary Design Optimization Framework with Coupled Derivative Computation for Hybrid Aircraft

    Sgueglia, Alessandro / Schmollgruber, Peter / Bartoli, Nathalie et al. | AIAA | 2020