Synonyms were used for: aircraft conference design lift
Search without synonyms: title: Vertical lift aircraft design conference

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    Baseline Design of Propeller for an eVTOL Aircraft to Achieve Urban Air Mobility

    Faraaz, Mohammed / Faizan, Afreed / Badarinath, Mukunda et al. | IEEE | 2023
    . Multiple configurations such as coaxial tilt-rotor and hybrid lift + cruise were considered for the aircraft, and preliminary design calculations ...

    Closed Blended Wing Body Concept Aircraft

    Jain, Aman / Biswas, Agniv / Saha, Soumik et al. | Springer Verlag | 2023
    adopted the Traditional Aircraft Wing Body (TAW) as the basis of aircraft designDesign. But it has its own ...
    Keywords: Lift-to-drag ratio

    Modeling and Control Optimization of the Shaft Driven Lift Fan Engagement

    Jiang, Tianmu / Zhang, Xiaobo / Wang, Zhanxue | IEEE | 2023
    key component for short takeoff and vertical landing (STOVL) aircraft. Through lift fan engagement, the propulsion system can obtain high ...

    A Landing Dynamics Analysis Model For STOVL Aircraft

    Sivrioglu, Selim | IEEE | 2023
    This study focuses on the landing dynamics of a short takeoff and vertical landing (STOVL) aircraft from a modeling perspective. The ...

    Design of a Quad-Jet VTOL UAS for Heavy-lift Applications

    Turkmen, Abdullah / Altug, Erdinc | IEEE | 2020
    this paper, we propose a Quad-Jet VTOL (vertical take-off and land) UAS with a thrust system consisting of four mini jet engines. Such a ...

    AIAA-2019-3478: Lift Fan Assessment for Conceptual Design of Aircraft Forebody

    Myers, Leighton / Czerwiec, Ryan / Napolillo, Zachary | British Library Conference Proceedings | 2019

    Research on Structural and Aeroelastic Design of a Hybrid Multi-rotor UAV

    Yang, Chuanguang / Ma, Tielin / Zhang, Zilun et al. | IEEE | 2019
    The structural design of a Hybrid Multi-rotor UAV which is aimed to have both conventional take-off and landing (CTOL) and vertical take ...

    Numerical and Experimental Second Law Analysis of a Low Thickness High Chamber Wing Profile

    Trancossi, Michele / Sharma, Shivesh | SAE Technical Papers | 2018
    interesting performances that can be exploited for the design of low-speed STOL or VTOL aircraft by mean of the very high lift that it can generate ...
    Keywords: Vertical take-off and landing (VTOL) , Aircraft

    Metrics for NASA Aeronautics Research Mission Directorate (ARMD) Strategic Thrust 3B Vertical Lift Strategic Direction

    Hochstetler, Ronald D. / Salvano, Dan / Gorton, Susan A. | NTRS | 2017
    Strategic Thrust Area 3B "Vertical Lift Strategic Direction." ...
    Keywords: Aircraft Design, Testing And Performance

    Anti-skid braking control system design for aircraft: Multi-phase schemes approach

    Lonbani, Mohammadali Aghakhani / Morandini, Marco / Astori, Paolo et al. | IEEE | 2017
    A multiphase approach is considered for the design of an aircraft anti-skid braking control system. A four-phase scheme, based on angular ...

    Analytical model and control solutions for unmanned aerial vehicle maneuvers in a vertical plane

    Azimov, Dilmurat / Allen, John | IEEE | 2017
    In this study, we present a class of nonlinear analytical solutions for the dynamics of a fixed wing unmanned aircraft vehicle (UAV). These ...

    Attitude and velocity high-gain control of a tilt-trirotor UAV

    Canciello, Giacomo / Cavallo, Alberto / D'Amato, Egidio et al. | IEEE | 2017
    for fixed wing tilt rotors in view of the lift control during transition from hovering to forward flight. The nonlinear dynamics, the large ...

    Large-Scale V/STOL Experimental Investigations of an Ejector-Lift Fighter and a Twin Tilt-Nacelle Transport

    Dudley, Michael R. | NTRS | 2016
    -mounted thrust augmenting ejector and a ventral deflecting jet nozzle for vertical lift. The Grumman Aircraft Company, the Navy, and NASA ...
    Keywords: Aircraft Design, Testing And Performance , Powered Lift

    Coaxial Compound Helicopter for Confined Urban Operations

    Johnson, Wayne / Elmore, Joshua F. / Keen, Ernest B. et al. | NTRS | 2016
    off-load the rotors at high speed, and ducted fans under the rotor disk for propulsion. The baseline design is described, and the aircraft ...
    Keywords: Aircraft Design, Testing And Performance

    Hover Testing of a Large Multi-Element Arc Wing VTOL Research Model

    Bertelsen, William D. | SAE Technical Papers | 2016
    Technology to create a VTOL for general aviation that is fast, efficient, easy to fly, and affordable, has proven elusive. Bertelsen Design ...
    Keywords: Vertical take-off and landing (VTOL) , Aircraft

    Advanced Vertical Lift Aircraft Demonstrator: Design for Certification of a Hover Lift-Drive System

    Silva-Martinez, Jackelynne P. / Lee, Woobong / Boshinski, Andrew | AIAA | 2015

    Advanced Vertical Lift Aircraft Demonstrator: Design for Certification of a Hover Lift-Drive System (AIAA 2015-0974)

    Silva-Martinez, Jackelynne P. / Lee, Woobong / Boshinski, Andrew | British Library Conference Proceedings | 2015

    On estimation of wind velocity, angle-of-attack and sideslip angle of small UAVs using standard sensors

    Johansen, Tor A. / Cristofaro, Andrea / Sorensen, Kim et al. | IEEE | 2015
    estimate and vertical accelerometer measurements, as would be expected since lift force can be modeled as a linear function of AOA in normal flight. ...

    Trust Control of VTOL Aircraft Part Deux

    Dugan, Daniel C. | NTRS | 2014
    Thrust control of Vertical Takeoff and Landing (VTOL) aircraft has always been a debatable issue. In most cases, it comes down to the ...
    Keywords: Aircraft Design, Testing And Performance , Aircraft controls , VTOL Aircraft

    Analysis of advanced flight management systems (FMSS), Flight management computer (FMC) field observations trials: Performance based navigation to X landing system (PBN to xLS)

    Herndon, Albert / Cramer, Michael / Miller, Sam et al. | IEEE | 2014
    current aircraft/avionics that might be used to fly them over a range of design and environmental conditions. The approach chosen for this ...