Synonyms were used for: Aircraft Design
Search without synonyms: title: Aircraft Aerodynamic Design

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    Preliminary Design of a Model-Free Synthetic Sensor for Aerodynamic Angle Estimation for Commercial Aviation

    Free access
    Lerro / Brandl / Battipede et al. | BASE | 2019
    bring analytical sensors on board of civil aircraft as part of a redundant system for the very first time, design activities documented in this ...

    Initial Weight Estimation of Twin Fuselage Configuration in Aircraft Conceptual Design

    Free access
    Ma, Yiyuan / Yan, Jin / Elham, Ali | BASE | 2021
    The Ultra High Aspect Ratio Wing (UHARW) concept can improve the aircraft 's aerodynamic efficiency and reduce fuel consumption. T he Twin ...
    Keywords: aircraft conceptual design

      Initial Weight Estimation of Twin Fuselage Configuration in Aircraft Conceptual Design

      Free access
      Ma, Yiyuan / Yan, Jin / Elham, Ali | BASE | 2021
      The Ultra High Aspect Ratio Wing (UHARW) concept can improve the aircraft 's aerodynamic efficiency and reduce fuel consumption. T he Twin ...
      Keywords: aircraft conceptual design

    Multi-Fidelity Design Optimization of a Long-Range Blended Wing Body Aircraft with New Airframe Technologies

    Free access
    Karpuk, Stanislav / Liu, Yaolong / Elham, Ali | BASE | 2020
    optimized using the multi-fidelity aircraft design code SUAVE with a connection to the Computational Fluid Dynamics (CFD) code SU2. The conceptual ...
    Keywords: aircraft design -- aerodynamics -- aerodynamic design optimization -- blended wing body -- new airframe technologies

      Multi-Fidelity Design Optimization of a Long-Range Blended Wing Body Aircraft with New Airframe Technologies

      Free access
      Karpuk, Stanislav / Liu, Yaolong / Elham, Ali | BASE | 2020
      optimized using the multi-fidelity aircraft design code SUAVE with a connection to the Computational Fluid Dynamics (CFD) code SU2. The conceptual ...
      Keywords: aircraft design -- aerodynamics -- aerodynamic design optimization -- blended wing body -- new airframe technologies

    Aerodynamic Analysis with Athena Vortex Lattice (AVL)

    Free access
    Budziak, Kinga | BASE | 2015
    Publisher: Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences , Institutional Repository of Leibniz Universität Hannover
    Keywords: aircraft , Luftfahrzeug

    Design Investigation of Potential Long-Range Hydrogen Combustion Blended Wing Body Aircraft with Future Technologies

    Free access
    Karpuk, Stanislav / Ma, Yiyuan / Elham, Ali | BASE | 2023
    multi-disciplinary optimizations. To assess potential uncertainties of the fidelity of aerodynamic analysis tools, high-fidelity aerodynamic ...
    Keywords: blended wing body -- aircraft design -- sustainable aviation -- multidisciplinary design optimization -- aircraft performance

    Conceptual Design and Comparative Study of Strut-Braced Wing and Twin-Fuselage Aircraft Configurations with Ultra-High Aspect Ratio Wings

    Free access
    Ma, Yiyuan / Karpuk, Stanislav / Elham, Ali | BASE | 2021
    ratio wings (UHARW) configuration is one key enabling strategy for improving aircraft aerodynamic efficiency and reducing fuel consumption and ...

      Conceptual Design and Comparative Study of Strut-Braced Wing and Twin-Fuselage Aircraft Configurations with Ultra-High Aspect Ratio Wings

      Free access
      Ma, Yiyuan / Karpuk, Stanislav / Elham, Ali | BASE | 2021
      ratio wings (UHARW) configuration is one key enabling strategy for improving aircraft aerodynamic efficiency and reducing fuel consumption and ...

    Dual-axis tilting quadrotor aircraft: Dynamic modelling and control of dual-axis tilting quadrotor aircraft

    Free access
    Von Klemperer, Nicholas | BASE | 2018
    work is plant model identification and control solution of the proposed aircraft design. A higher-level setpoint tracking control loop designs ...

    Fuzzy Logic Control for Aircraft Longitudinal Motion

    Free access
    Narenathreyas, Kashyapa Bramha | BASE | 2013
    Aircraft design consists of many steps such as aerodynamic design, structural analysis and flight control design etc. and flight control is ...
    Keywords: Aircraft Longitudinal motion

    Flutter Characteristics of Typical Wing Sections of a Box Wing Aircraft Configuration

    Free access
    Fazelzadeh, S. Ahmad / Scholz, Dieter / Mazidi, Abbas et al. | BASE | 2018
    simulation on the box wing, the Theodorsen aerodynamic model is used. The effects of various design parameters such as front and rear wing physical ...
    Keywords: aircraft design , Luftfahrzeug

    Aeroelasticity model for highly flexible aircraft based on the vortex lattice method

    Free access
    Dagilis, Mindaugas / Kilikevičius, Sigitas | BASE | 2023
    With the increasing use of composite materials in aviation, structural aircraft design often becomes limited by stiffness, rather than ...

    Reverse Engineering of Passenger Jets – Classified Design Parameters

    Free access
    De Grave, Emiel | BASE | 2017
    This thesis explains how the classified design parameters of existing passenger jets can be determined. The classified design parameters ...
    Publisher: Hamburg : Aircraft Design and Systems Group (AERO), Department of Automotive and Aeronautical Engineering, Hamburg University of Applied Sciences , Institutional Repository of Leibniz Universität Hannover
    Keywords: Luftfahrzeug , Design

    Conceptual Design of an Ekranoplan UAV ; Konceptuell utformning av Ekranoplan UAV

    Free access
    Yu, Sheng-An | BASE | 2022
    , pollution forensics and geographic monitoring. This thesis work aims to design a unmanned ground effect vehicle (UGEV) in order to provide a much ...
    Keywords: aircraft design

    Application of the Piloting Law Based on Adaptive Differentiators via Second Order Sliding Mode for a Fixed Wing Aircraft

    Free access
    Zaouche Mohammed / Amini Mohammed / Foughali Khaled et al. | BASE | 2016
    In this paper, we present a piloting law based on the adaptive differentiators via high order sliding mode controller, by using an aircraft ...

    Preliminary design of a Tiltwing UAV with a box wing configuration

    Free access
    Giuseppe Palaia / Karim Abu Salem / Vittorio Cipolla et al. | BASE | 2018
    In the last years, aircraft disruptive configurations have been studied on view to increase civil air transport and safety of flight and ...

    Integrated Flight Control System Characterization Approach for Civil High-Speed Vehicles in Conceptual Design

    Free access
    Ferretto, Davide / Gori, Oscar / Fusaro, Roberta et al. | BASE | 2023
    Recent studies have revealed that control surface deflection can cause a reduction in the aerodynamic efficiency of a hypersonic aircraft ...
    Keywords: flight control system design

    Design and experimental testing of a control system for a morphing wing model actuated with miniature BLDC motors

    Free access
    Grigorie, Teodor Lucian / Khan, Shehryar / Botez, Ruxandra Mihaela et al. | BASE | 2019
    The paper deals with the design and experimental validation of the actuation mechanism control system for a morphing wing model. The ...

    Design of Efficient High-Lift Configurations with Coanda Flaps ; Entwicklung effizienter Hochauftriebskonfigurationen mit Coanda Klappen

    Free access
    Burnazzi, Marco | BASE | 2017
    -less droop-nose design are presented, describing the aerodynamic sensitivities of the main geometrical parameters and the physical phenomena ...

      Design of Efficient High-Lift Configurations with Coanda Flaps ; Entwicklung effizienter Hochauftriebskonfigurationen mit Coanda Klappen

      Free access
      Burnazzi, Marco | BASE | 2017
      -less droop-nose design are presented, describing the aerodynamic sensitivities of the main geometrical parameters and the physical phenomena ...

    Modeling, design, and flight testing of three flutter controllers for a flying-wing drone

    Free access
    Schmidt, David K. / Danowsky, Brian P. / Kotikalpudi, Aditya et al. | BASE | 2020
    flight research into the modeling and control of highly elastic aircraft. The lowspeed vehicle was designed to exhibit body-freedom flutter in ...

    Drag Reduction by Laminar Flow Control

    Free access
    Beck, Nils / Landa, Tim / Seitz, Arne et al. | BASE | 2018
    ) solver. The effect on total aircraft drag is estimated for a state-of-the-art mid-range aircraft configuration using preliminary aircraft design ...
    Keywords: drag reduction -- laminar flow control -- boundary layer suction -- transition -- aircraft design

      Drag Reduction by Laminar Flow Control

      Free access
      Beck, Nils / Landa, Tim / Seitz, Arne et al. | BASE | 2018
      ) solver. The effect on total aircraft drag is estimated for a state-of-the-art mid-range aircraft configuration using preliminary aircraft design ...
      Keywords: drag reduction -- laminar flow control -- boundary layer suction -- transition -- aircraft design

    Coupling Mid-Fidelity Aerodynamics and Multibody Dynamics for the Aeroelastic Analysis of Rotary-Wing Vehicles

    Free access
    Savino, Alberto / Cocco, Alessandro / Zanotti, Alex et al. | BASE | 2021
    aerodynamic approach represents an effective trade-off in obtaining fast and accurate solutions that can be used for the preliminary design of novel ...