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

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    발사 시스템

    Free access
    PELEG EYAL / VALENCY TOMER / BARBOI ILAN | European Patent Office | 2021
    제공하도록 설계된 탑재 추진 시스템(payload propulsion system) 및 공기 역학적 부상 표면들(aerodynamic lift surfaces)을 포함한다. 수송체는 적어도 하나의 탑재체를 적어도 목적하는 고도까지 수송하도록 구성되고, 발사 ...

    Workstation for the integrated design and simulation of flight control systems

    Colgren, R.D. | Tema Archive | 1989
    The development of a workstation that integrates design, analysis, and simulation methods used for flight control system synthesis is ...
    Keywords: AIRCRAFT CONTROL

    Voltage doubling rectifier for electric aerodynamic propulsion high-voltage power supply

    Free access
    ZHAO ZHENXING / LI BOYUE / LIU ZENG et al. | European Patent Office | 2022
    the weight of the LCC converter can be achieved, and the lightweight design requirement of an aircraft can be met. ...

    Versatile, modular, extensible vtol aerial platform with autonomous flight mode transitions

    Sinha, Pranay / Esden-Tempski, Piotr / Forrette, Christopher A. et al. | IEEE | 2012
    maneuverability is achieved via a combination of differential thrust and aerodynamic surfaces (elevons). The relaxed stability, flying wing, tail-sitter ...

    Variable structure robust flight control system for the F-14

    Singh, S.N. / Steinberg, M. / DiGirolamo, R.D. | IEEE | 1997
    In this paper, a flight control law for a simplified F-14 aircraft model is designed based on variable structure control (VSC) theory. For ...

    Tracked Air Cushion Research Vehicle. Volume III Research Vehicle Research Plan

    NTIS | 1969
    design of a public demonstration system. The TACRV will be used to obtain test operation data, under actual forward speed conditions, in the ...
    Publisher: Grumman Aircraft Engineering Corp., Bethpage, N. Y
    Keywords: Aerodynamic characteristics

    Towards Complete Configurations Using an Embedded Grid Approach

    C. W. Boppe | NTIS | 1978
    illustrate aspects of transonic transport design including fuselage design, determination of wing control surface deflection effectiveness, and wing ...
    Keywords: Aircraft , Aerodynamic characteristics

    Towards bio-inspired structural design of a 3D printable, ballistically deployable, multi-rotor UAV

    Henderson, Luke / Glaser, Twain / Kuester, Falko | IEEE | 2017
    This paper explores bio-inspired design strategies to guide the structural design of a 3D printable, foldable and ballistically deployable ...

    The SOFIA aircraft and its modification

    Kunz, N. | Tema Archive | 2003
    The primary focus of this paper is to describe the development of a highly modified aircraft that carries a twenty ton telescope to the ...
    Keywords: Luftfahrzeug

    Thermal management of military fighter aircraft electro-optics pod: an invited paper

    Price, D.C. | Tema Archive | 2003
    The thermal management of electro-optics equipment mounted in a pod residing under the fuselage of a fighter aircraft represents a ...

    The Development of a Small Solar Powered Electric Unmanned Aerial Vehicle Systems

    Rajendran, Parvathy / Smith, Howard | Tema Archive | 2013
    studies on the design of a solar and battery power system for an electric UAV. Subsequently, a small solar powered electric UAV has been developed ...
    Keywords: unbemanntes Luftfahrzeug

    The Development of a Small Solar Powered Electric Unmanned Aerial Vehicle Systems

    Rajendran, Parvathy / Smith, Howard | Trans Tech Publications | 2013
    studies on the design of a solar and battery power system for an electric UAV. Subsequently, a small solar powered electric UAV has been developed ...
    Keywords: Unmanned Aircraft Systems

    Summary of Rotochute Development

    D. W. Robinson | NTIS | 1956
    Publisher: Kaman Aircraft Corp., Bloomfield, CT
    Keywords: Aerodynamic characteristics , Design

    Special problems associated with aircraft radomes

    Conti, D.A. | Tema Archive | 1981
    The paper discusses the design and manufacturing aspects of nose radomes for high-speed aircraft. Aircraft radomes are an acceptable ...

    Simulation based aerodynamic design

    Jameson, A. / Martinelli, L. / Alonso, J.J. et al. | IEEE | 2000
    This paper reviews the status of advanced computational simulation techniques in the aerodynamic design of modern aircraft. An outline of ...

    Screening and shielding in aircraft - the balanced approach

    MacDiarmid, I.P. | Tema Archive | 1983
    remains a problem of unknown extent. Airframe designers traditionally considered the dtructural strength of the design along with the aerodynamic ...

    Sabot High Speed Interceptor AE 4273 Aircraft Design

    D. Dober / W. Al-hashel / B. Baldocchi et al. | NTIS | 1992
    which contains design requirements for an aircraft that can complete this mission through the utilization of waverider technology. ...
    Keywords: Aircraft , Aircraft design , Fighter aircraft , Jet aircraft , Supersonic aircraft , Aerodynamic characteristics , Aircraft control , Aircraft performance , Aircraft structures

    QFT force loop design for the aerodynamic load simulator

    Yoonsu Nam, | IEEE | 2001
    A dynamic load simulator which can reproduce on-ground the aerodynamic hinge moment of a control surface is an essential rig for conducting ...

    Performance Trade-offs and Operations of Electric Boosted Aircraft for 2030 Single-Aisle Market

    Balkas, Ezgi / Shi, Mingxuan / Gladin, Jonathan C. et al. | IEEE | 2022
    benefits and better take-off performance. Existing in-house tools have been updated for turboelectric hybrid aircraft design and leverage the ...