1–20 von 21 Ergebnissen
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    The Pilot Influence on the Flutter Velocity of the Lightweight Plane

    Freier Zugriff
    Sommer Tomáš / Steinbauer Pavel / Slavík Svatomír et al. | DOAJ | 2019
    Flutter of the airplane is serious problem which is carefully investigated during design and testing both computationally and ...

    Considerations on the role of modernizing the road infrastructure in the prevention of road accidents

    Freier Zugriff
    Deac Cristian / Tarnu Lucian | DOAJ | 2019
    The realizing and improvement of road infrastructure, of modern road networks provides normal, safe and pleasant road traffic conditions ...

    Simulating of Bird Strike on Aircraft Laminated Glazing

    Freier Zugriff
    Smetankina Natalia / Malykhina Alyona / Merkulov Dmytro | DOAJ | 2019
    A bird strike is a critical problem in the context of safety in the aviation industry. All modern aircraft structures are designed with ...

    Parametric Design Study on Aerodynamic Characteristics of Variable Pitot Inlets for Transonic and Supersonic Civil Aviation

    Freier Zugriff
    Kazula Stefan / Wöllner Mark / Grasselt David et al. | DOAJ | 2019
    This paper reveals the influence of selected geometric parameters on the aerodynamic performance of circular variable aero engine inlets in ...

    Flight Test of Pilot-Aircraft Haptic Feedback System

    Freier Zugriff
    Zikmund Pavel / Dubnický Lukáš / Horpatzká Michaela et al. | DOAJ | 2019
    This research is focused on an innovative improvement of pilot-aircraft interaction and is targeted on small aircraft. Haptic feedback is ...

    Design of distributed propulsion system for general aviation airplane

    Freier Zugriff
    Hospodář Pavel / Klesa Jan / Žižkovský Nikola | DOAJ | 2019
    the reduction of fuel consumption in cruise regime with constrained parameters of take-off/landing. In this case, a one half wing area ...

    Effects of Propeller Slipstream of Distributed Electric Propulsion on the Wing-Flap System

    Freier Zugriff
    Mikhalyov Semyon / Dunaevsky Andrey / Teperin Leonid et al. | DOAJ | 2019
    The studies are aimed at investigating the mechanism to ensure the high lift by installing propellers in front of the wing and using ...

    Powered wind tunnel tests setup of the IRON innovative turboprop aircraft

    Freier Zugriff
    Ciliberti Danilo / Cusati Vincenzo / Della Vecchia Pierluigi et al. | DOAJ | 2019
    This paper describes the powered wind tunnel tests setup of the innovative configuration of the IRON regional turboprop aircraft. The ...

    Assessment of the performance of a cruise missile wing depending on design parameters at various flight conditions

    Freier Zugriff
    Erturk Burak / Yaman Yavuz | DOAJ | 2019
    The design of a cruise missile wing is a multidisciplinary work, since the wing has to provide enough aerodynamic forces while being ...

    Analysis of a combined cycle propulsion system for STRATOFLY hypersonic vehicle over an extended trajectory

    Freier Zugriff
    Ispir Ali Can / Gonçalves Pedro Miguel / Saracoglu Bayindir H. | DOAJ | 2019
    , are proposed to achieve high-speed civil air transportation. STRATOFLY project is a continuation of former European efforts in hypersonic ...

    Development of a robust solver to model the flow inside the engines for high-speed propulsion

    Freier Zugriff
    Nista Ludovico / Saracoglu Bayindir H. | DOAJ | 2019
    of civil hypersonic vehicle designs. Among all the multiple projects started by the various nations, the European community funded project ...

    Aerodynamic moment characteristics of tandem-scheme aircraft

    Freier Zugriff
    Kryvokhatko Illia | DOAJ | 2019
    Aerodynamic interference between forward and back wings of tandem-scheme aircraft significantly affects its pitch and roll moments. The ...

    The concept and methodical assumptions for the development of dynamically scaled aircraft model (passenger aircraft)

    Freier Zugriff
    Olejnik Aleksander / Kachel Stanisław / Rogólski Robert et al. | DOAJ | 2019
    The article describes the concept of scaled model and its application in the process of real aircraft prototyping. Computer simulations of ...

    Stability study and flight simulation of a blended-wing-body UAV

    Freier Zugriff
    Dimopoulos Thomas / Panagiotou Pericles / Yakinthos Kyros | DOAJ | 2019
    This article is a product of the design process of a Blended-Wing- Body Unmanned Aerial Vehicle (BWB UAV). The BWB geometry blends the wing ...

    Towards the harmonisation of Just Culture across organisations: the London Luton Airport case

    Freier Zugriff
    Kirwan Barry / Bettignies-Thiebaux Beatrice / Bolger Liam | DOAJ | 2019
    enacted, including the openness of the culture, the investigation processes, and the degree of authentic support from senior and middle management ...

    GICS, a new concept to enhance in-flight safety and security of commercial aviation

    Freier Zugriff
    Lesturgie Marc / Chan Hian Lim / Azarian Sylvain | DOAJ | 2019
    This paper presents a new concept of aircraft tracking based on a LEO constellation of small satellites, each of them carrying receiving ...

    Optimal civil aircraft missions exploiting free routing possibilities

    Freier Zugriff
    Katsikogiannis Dimitrios / Thoma Marily / Mathioudakis Konstantinos et al. | DOAJ | 2019
    A method is presented for optimizing burnt fuel and flight time of civil aircraft missions, under the scope of a full-scale free route ...

    Navigation architecture for hypersonic aircraft

    Freier Zugriff
    Castigliola Luca / Causa Flavia / Grassi Michele | DOAJ | 2019
    This paper aims at presenting an integrated navigation algorithm designed for estimating the navigation state of the STRATOFLY vehicle ...

    How many RPAS can be safely integrated in non–segregated airspace?

    Freier Zugriff
    Pérez–Castán Javier A. / Gómez Comendador Fernando / Rodriguez–Sanz Alvaro et al. | DOAJ | 2019
    The forthcoming integration of Remotely Piloted Aircraft System (RPAS) is one of the cmost omplex challenges for aviation. Europe draws to ...

    Wing-Propeller Interaction

    Freier Zugriff
    Zizkovsky Nikola / Klesa Jan | DOAJ | 2019
    Paper describes the effect of the distributed electric propulsion system (DEP) on the aerodynamic characteristics of the airplane wing ...