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Nguyen, Nhan T.   Mor, Marat   Verkehrstechnik, Verkehrswesen   Geowissenschaften, Geographie   Englisch   Auswahl aufheben

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Suche ohne Synonyme: title: AIAA Scitech 2020 Forum

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    ACOUSTIC OPTIMIZATION FOR ANTI-PHASE ASYMMETRIC ROTOR

    Xiong, Juntao / Nguyen, Nhan T. / Cramer, Nick B. | TIBKAT | 2020

    Development of an Aeroservoelastic Model for Gust Load Alleviation of the NASA Common Research Model Wind Tunnel Experiment

    Cramer, Nick B. / Nguyen, Nhan T. | AIAA | 2020

    Jig Twist Optimization of Mach 0.745 Transonic Truss Braced Wing Aircraft and High-Fidelity CFD Validation

    Xiong, Juntao / Fugate, Jason A. / Nguyen, Nhan T. | AIAA | 2020

    Mode-based Sensing and Actuation Techniques for Multi-objective Flexible Aircraft Control

    Hashemi, Kelley E. / Alder, Andrew / Cramer, Nick B. et al. | AIAA | 2020

      MODE-BASED SENSING AND ACTUATION TECHNIQUES FOR MULTI-OBJECTIVE FLEXIBLE AIRCRAFT CONTROL

      Hashemi, Kelley E. / Alder, Andrew / Cramer, Nick B. et al. | TIBKAT | 2020

      Mode-Based Sensing and Actuation Techniques for Multi-Objective Flexible Aircraft Control

      Hashemi, Kelley E. / Alder, Andrew / Cramer, Nick et al. | NTRS | 2020

    Modeling of Electric Reeling Systems in Aerial Refueling Hose Pods Using Matlab/Simulink

    Chaturvedi, Arnav / Mor, Marat / Erickson, Andrew J. et al. | AIAA | 2020

      MODELING OF ELECTRIC REELING SYSTEMS IN AERIAL REFUELING HOSE PODS USING MATLAB/SIMULINK

      Chaturvedi, Arnav / Mor, Marat / Erickson, Andrew J. et al. | TIBKAT | 2020

    MODEL-REFERENCE ADAPTIVE CONTROL OF DISTRIBUTED LAGRANGIAN INFINITE- DIMENSIONAL SYSTEMS USING HAMILTON'S PRINCIPLE.

    Nguyen, Nhan T. / Hashemi, Kelley E. / Arabi, Ehsan et al. | TIBKAT | 2020

    MODEL REFERENCE ADAPTIVE CONTROL OF UNCERTAIN DYNAMICAL SYSTEMS SUBJECT TO HIGH-ORDER ACTUATOR DYNAMICS WITH PERFORMANCE GUARANTEES

    Arabi, Ehsan / Panagou, Dimitra / Yucelen, 1ansel et al. | TIBKAT | 2020

    Multi-Objective Flight Control for Ride Quality Improvement for Flexible Aircraft

    Nguyen, Nhan T. / Hashemi, Kelley E. | AIAA | 2020

    Multi-Objective Gust Load Alleviation Control Designs for an Aeroelastic Wind Tunnel Demonstration Wing

    Drew, Michael C. / Hashemi, Kelley E. / Cramer, Nick B. et al. | AIAA | 2020

      MULTI-OBJECTIVE GUST LOAD ALLEVIATION CONTROL DESIGNS FOR AN AEROELASTIC WIND TUNNEL DEMONSTRATION WING

      Drew, Michael C. / Hashemi, Kelley E. / Cramer, Nick B. et al. | TIBKAT | 2020

    Progress on Gust Load Alleviation Wind Tunnel Experiment and Aeroservoelastic Model Validation for a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System

    Nguyen, Nhan T. / Cramer, Nick B. / Hashemi, Kelley E. et al. | AIAA | 2020

      PROGRESS ON GUST LOAD ALLEVIATION WIND TUNNEL EXPERIMENT AND AEROSERVOELASTIC MODEL VALIDATION FOR A FLEXIBLE WING WITH VARIABLE CAMBER CONTINUOUS TRAILING EDGE FLAP SYSTEM

      Nguyen, Nhan T. / Cramer, Nick B. / Hashemi, Kelley E. et al. | TIBKAT | 2020

      Progress on Gust Load Alleviation Wind Tunnel Experiment and Aeroservoelastic Model Validation for a Flexible Wing with Variable Camber Continuous Trailing Edge Flap System

      Nguyen, Nhan / Cramery, Nicholas / Hashemiz, Kelley et al. | NTRS | 2020
      servos prevented the test objective from being completed. A follow-up second test entry in 2020 is being planned. The wing system is being ...

    SIMULATION AND MODELING OF FLOW GENERATED BY GUST GENERATOR IN A WIND TUNNEL

    Nguyen, Nhan T. / Xiong, Juntao / Cramer, Nick B. | TIBKAT | 2020

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