1–20 von 194 Ergebnissen
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    Wing Shaping Concept for Distributed Propulsion Aircraft to Improve Aerodynamic Efficiency

    Nguyen, Nhan T. / Reynolds, Kevin W. / Ting, Eric | AIAA | 2016

    Wall Pressure Fluctuations in an Over-Expanded Rocket Nozzle

    Nguyen, Anh / Deniau, H. / Girard, S. et al. | AIAA | 2002

    Wake Vortex Interaction of Urban Air Mobility Aircraft

    Nguyen, Nhan T. / Bartolini, Graeson / Baculi, Joshua E. et al. | AIAA | 2022

    Wake Vortex Effects Between Urban Air Mobility Aircraft

    Baculi, Joshua E. / Nguyen, Nhan T. / Okolo, Wendy et al. | AIAA | 2023

    Vortex modeling of single and multiple dilution jet mixing in a cross flow

    KARAGOZIAN, A. R. / NGUYEN, T. T. / KIM, C. N. | AIAA | 1986

    Use of a Viscous Flow Simulation Code for Static Aeroelastic Analysis of a Wing at High-Lift Conditions

    Akaydin, H. Dogus / Moini-Yekta, Shayan / Housman, Jeffrey A. et al. | AIAA | 2015

    Transonic and Viscous Potential Flow Method Applied to Flexible Wing Transport Aircraft

    Chaparro, Daniel / Fujiwara, Gustavo E. / Ting, Eric et al. | AIAA | 2017

    Time-Varying Weights in Multi-Objective Optimal Control for Flexible Wing Aircraft

    Hashemi, Kelley E. / Nguyen, Nhan T. / Drew, Michael C. | AIAA | 2019

    Time Delay Margin Analysis of Modified State Observer Based Adaptive Control

    Rajagopal, Karthikeyan / Balakrishnan, Sivasubramanya N. / Nguyen, Nhan T. et al. | AIAA | 2013

    The liquid fuel jet in subsonic crossflow

    NGUYEN, T. / KARAGOZIAN, A. | AIAA | 1990