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

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    Enhancement of an Aircraft Design Environment for the Design of Fighter Aircraft

    Hasenau, M.A.C. / Varga, S.A. / Scholz, A.E. et al. | DataCite | 2021
    aircraft. New design challenges were, among others, the approximation of the aerodynamic and geometrical effects of supersonic flight and increased ...
    Keywords: fighter aircraft , aircraft design

    Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level

    Effing, Tim / Peter, F. / Stumpf, Eike et al. | DataCite | 2022
    Keywords: Conceptual aircraft design

    Approach for the Aerodynamic Optimization of the Twist Distribution of Arbitrary Wing Geometries on Conceptual Aircraft Design Level

    Effing, T. / Peter, F. / Stumpf, E. et al. | DataCite | 2021
    This paper presents an approach for consciously tailoring the lift distribution of a given wing geometry in early stages of aircraft design ...
    Keywords: Conceptual aircraft design

    Aerodynamic Design and Wind Tunnel Test of a Laminar Wing with Split Flap for a Fuel Cell Powered Aircraft

    Free access
    Frey, J. / Sell, F. / Gillespy, R. et al. | DataCite | 2021
    This paper presents a wing design for the APUS i-2 concept hydrogen fuel cell aircraft that meets design requirements for hydrogen storage ...

    High-Lift-System Design for a Low-Noise Medium-Range Aircraft

    Free access
    Schmidt, F.N. / Keller, D. / Iwanizki, M. et al. | DataCite | 2024
    The DLR project "Low noise medium-range aircraft" (SIAM) has set itself the goal of designing an aircraft with the boundary conditions of ...
    Keywords: Aerodynamic Design , Low-Noise Aircraft

    Preliminary overall aircraft design with hybrid laminar flow control

    Risse, Kristof | DataCite | 2016
    This thesis deals with preliminary overall aircraft design including hybrid laminar flow control (HLFC) on wings and tails. An integrated ...
    Keywords: Flugzeugentwurf ; Aircraft Design ; Wing Design ; Hybrid Laminar Flow Control ; HLFC

    Initial Weight Estimation of Twin Fuselage Configuration in Aircraft Conceptual Design

    Ma, Yiyuan / Yan, Jin / Elham, Ali | DataCite | 2021
    The Ultra High Aspect Ratio Wing (UHARW) concept can improve the aircraft 's aerodynamic efficiency and reduce fuel consumption. T he Twin ...
    Keywords: Twin fuselage configurati on, initial weight estimation, vortex lattice m ethod, composite materials, aircraft conceptual design

    A Calculation Method for Over-the-Wing Engines within Conceptual Aircraft Design

    DataCite | 2019
    -wing engine installation effects in terms of lift, drag and structure weight at the conceptual stage of aircraft design. The aerodynamic ...
    Keywords: Conceptual Aircraft Design

    Design Study on Hydrogen Supersonic Transport Aircraft on the Basis of the Concorde

    Free access
    Türkyilmaz, B. / Scholz, A.E. / Chrzan, J.-M. et al. | DataCite | 2024
    , the aircraft design environment Aircraft Design Box (ADEBO) of TU Munich was modified for kerosene and hydrogen SST design. The modifications ...
    Keywords: Aircraft design , Liquid hydrogen powered aircraft , Supersonic transport aircraft

    Initial Assessment of Stability and Controllability in the Early Stage of Combat Aircraft Design

    Christmann, C. / Kiehn, D. / Stradtner, M. et al. | DataCite | 2021
    design. Requirements on stability and controllability are driving factors for the design of control effectors of a combat aircraft to ensure ...
    Keywords: combat aircraft design

    Design of a Hybrid-Electric Powertrain for a Next Generation VTOL Firefighting Aircraft from the DLR Design Challenge 2022

    Free access
    Ritter, J. / Mandry, N. / Can, G.A. et al. | DataCite | 2021
    indispensable safety aspects. Due to its modular design, every aircraft can be comfortably converted to a passenger or freight version during ...
    Keywords: aircraft design

    Actuated Adaptive Wingtips on Transport Aircraft: Requirements and Preliminary Design Using Pressure-Actuated Cellular Structures

    Free access
    Meyer, Patrick / Traub, Hendrik / Hühne, Christian | DataCite | 2022
    aircraft by increasing the wing’s aspect ratio in flight. While state of the art commercial aircraft, such as the Boeing 777X, are equipped with on ...

    Disciplinary Sub-Processes to Assess Low-Speed Performance and Noise Characteristics within an Aircraft Design Environment

    Fröhler, B. / Hesse, C. / Atanasov, G. et al. | DataCite | 2021
    The overall aircraft assessment is based on a wide range of disciplinary methodologies. In addition, a consistent aircraft design must be ...
    Keywords: Conceptual aircraft design , multidisciplinary design and analysis , Aircraft noise prediction

    Influence of a Detailed Mass Estimation for a Wing with known Flight Shape in Conceptual Overall Aircraft Design

    Effing, T. / Stephan, R. / Stumpf, E. | DataCite | 2023
    (VC) application exhibits—from an overall aircraft design perspective—minor differences in the flight shape and, thus, in the aerodynamic ...
    Keywords: Conceptual aircraft design , short-medium range aircraft

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

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

    Sizing Studies of Light Aircraft with Serial Hybrid Propulsion Systems

    Ludowicy, J. / Rings, R. / Finger, D.F. et al. | DataCite | 2018
    conventionally powered aircraft with similar specifications, by the means of initial sizing results. Studies on battery specific energy and aerodynamic ...
    Keywords: Aircraft Preliminary Sizing

    Sizing Studies of Light Aircraft with Parallel Hybrid Propulsion Systems

    Rings, R. / Ludowicy, J. / Finger, D.F. et al. | DataCite | 2018
    conventional aircraft, even with todays technological standards. However, several design aspects have to be taken into account to make full use of the ...
    Keywords: Aircraft Preliminary Sizing

    Electrical propulsion systems for civil transportation aircraft; 1. Auflage

    Hinz, Arne | DataCite | 2022
    aircraft. Thereby, a number of electrical engines replaces the conventional engine while neglecting aerodynamic effects. This enables direct ...

    Aircraft-scale application of active separation control at the pylon-wing junction

    Free access
    Schlösser, Philipp | DataCite | 2019
    the wind tunnel model design. The aerodynamic effect of this flow control actuator has been studied with the help of force and pressure ...

    The Flying V A new Aircraft Configuration for Commercial Passenger Transport

    Benad, J. | DataCite | 2015
    configuration proposal was made with this idea. This configuration was then compared with a reference aircraft. The idea is to arrange two cylindrical ...
    Keywords: unconventional aircraft configuration