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

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    Electro-aerodynamic thrust for fixed-wing aircraft propulsion

    Free access
    Gilmore, Christopher K. (Christopher Kenneth) | DSpace@MIT | 2017
    thesis considers electro-aerodynamic (EAD) propulsion, a form of in-atmosphere electrostatic propulsion, which requires no on-board propellant ...

    Development of an aerodynamic/RCS framework for the preliminary design of a hypersonic aircraft.
    Development of an aerodynamic/Radar Cross Section framework for the preliminary design of a hypersonic aircraft

    Free access
    Dicara, Daniel L | DSpace@MIT | 2006
    analysis. The intent is to optimize a hypersonic airbreathing aircraft design in terms of aerodynamic performance and RCS. Computational Fluid ...

    Integrated Aerodynamic and Control System Design of Oblique Wing Aircraft

    Morris, Stephen James | NTRS | 1990
    An efficient high speed aircraft design must achieve a high lift to drag ratio at transonic and supersonic speeds. In 1952 Dr. R. T. Jones ...
    Keywords: Aircraft Stability And Control

    Design of a model propulsor for a boundary layer ingesting aircraft

    Free access
    Grasch, Adam D. (Adam Davis) | DSpace@MIT | 2013
    of work on propulsion system scaling, nacelle and flowpath aerodynamic optimization, mechanical design of the propulsor and characterization ...

    A flexible wing modeling and physical mass estimation system for early aircraft design stages

    Free access
    Dorbath, Felix / Technische Universität Hamburg-Harburg, Institut für Lufttransportsysteme | TIBKAT | 2014
    capability and models for aerodynamic, fuel, landing gear and engine loads. The chain is calibrated against two reference aircraft. The calibration ...
    Keywords: preliminary aircraft design

      A Flexible Wing Modeling and Physical Mass Estimation System for Early Aircraft Design Stages

      Dorbath, Felix | Tema Archive | 2014
      Keywords: Luftfahrzeug , Design-Umgebung

    Conceptual aircraft design for environmental impact : modeling operations for emissions assessment

    Free access
    King, Daniel J., S.M. Massachusetts Institute of Technology | DSpace@MIT | 2005
    economics for conceptual design of future aircraft. A key component to EDS is modeling the emissions of aircraft in operation. Traditional design ...

    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 ...

    The Aerodynamic Optimization of Wings at Subsonic Speeds and the Influence of Wingtip Design

    Zimmer, H. | NTRS | 1987
    investigation is mainly concerned with the aerodynamic aspects of aircraft development, i.e., reduction of induced drag. New studies of wing design, and ...

    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

    Influence of low-speed aerodynamic performance on airport community noise

    Free access
    March, Andrew I. (Andrew Irving) | DSpace@MIT | 2008
    preliminary phase of aircraft design. The goal of this thesis is to use the low-speed aerodynamic estimates to present the sensitivity of aircraft ...

    Shock control bumps on transonic transport aircraft

    König, Benedikt | Tema Archive | 2014
    current generation of aircraft. And from an aerodynamic point of view this means reducing the airframe drag. Current long range aircraft travel in ...
    Keywords: Luftfahrzeug , Industrie-Design

    Advances in Aero-Propulsive Modeling for Fixed-Wing and eVTOL Aircraft Using Experimental Data

    Benjamin M. Simmons | NTRS | 2023
    , tandem tilt-wing, eVTOL aircraft, leveraging design of experiments and response surface methodology techniques. Additionally, a method applying ...
    Keywords: design of experiments , Aircraft Design, Testing and Performance , Aircraft Stability and Control , aerodynamic modeling

    Analysis methods for novel cargo aircraft concepts

    Tang, S. | Tema Archive | 2002
    several novel air cargo system configurations with a dedicated freighter aircraft as a major element. In this contribution a consistent ...
    Keywords: CAD (Computer Aided 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

    A CFD/CSD Interaction Methodology for Aircraft Wings

    Bhardwaj, Manoj K. | NTRS | 1997
    effects of the coupling between aerodynamic loads and elastic forces. Since aeroelastic effects can contribute significantly to the design of ...

    Studies in tilt-rotor VTOL aircraft aeroelasticity, volume 1

    Kvaternik, R. G. | NTRS | 1973
    Aeroelastic and dynamic studies which complement and extend various aspects of technology applicable to tilt-rotor VTOL aircraft are ...

    Integrated strain actuation in aircraft with highly flexible composite wings

    Free access
    Brown, Eric L. (Eric Lee) | DSpace@MIT | 2003
    into account in the calculation of aerodynamic loads. The strain-based finite element formulation allows for a simplified control design ...

    Propeller design and analysis for a small, autonomous UAV

    Free access
    Tracy, Ian P | DSpace@MIT | 2011
    aerodynamic efficiency given a conservative aerodynamic design point. The TA22 airfoil defined the propeller cross section and NEU-012-030-4000 DC ...

    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 ...