Showing 1 - 20 results of 495 for search '"fuselage"', query time: 0.07s Refine Results
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    FUSELAGE SHAPE OPTIMIZATION AIMED AT WING-FUSELAGE CONFIGURATION DRAG REDUCTION AT SUPERSONIC SPEEDS by N. D. Ageev, A. A. Pavlenko

    Published 2017-01-01
    “…The problem of fuselage shape optimization of the wing-body configuration is considered in the following three formulations. …”
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    Article
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    Pressure distribution on helicopter fuselage by Aris, Anas Faiz, Ishak, Iskandar Shah, Ali, Airi, Othman, Norazila

    Published 2019
    “…Results also indicate the pressure distributions on the right and left sides of the fuselage are unsymmetrical indicating a very complex flow phenomenon experienced by the helicopter fuselage.…”
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    Article
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    Structural Health Monitoring of Helicopter Fuselage by Robert Hudec, Ladislav Janousek, Miroslav Benco, Pavol Makys, Vladimir Wieser, Martina Zachariasova, Matej Pacha, Vladimir Vavrus, Martin Vestenicky

    Published 2013-06-01
    “…The work presented in this paper is a part of an international research project HECTOR (HElicopter fuselage Crack moniToring and prognosis through On-board sensoR network), founded by the European Defense Agency (EDA) and supported by 10 EDA Member States: Cyprus, France, Germany, Greece, Hungary, Italy, Poland, Slovakia, Slovenia and Spain.…”
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    Article
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    ASSEMBLY OF THE PRIMARY STRUCTURE OF AN AIRPLANE FUSELAGE by Theodor Petrisor RUSOIU, Eng., Ionel SIMION, Ph.D. Eng.

    Published 2018-10-01
    “…Also, the fuselage holds cargo transports, luggage and, most important, passengers. …”
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    Article
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    Calculation of longitudinal forces acting on aircraft fuselage / by 430131 Phoon, Kin Wah

    Published 1993
    “…The final results shown as Critical Envelop of Shear Force and Bending Moment Diagram are fair indication of the longitudinal forces acting on fuselage of conventional light civil aircraft.…”
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    Educational software for stress analysis of an aircraft fuselage by Mohamed Ali, Jaafar Syed, Mustafa Kamal, Izyan Liyana, Ismail, Nurhuda

    Published 2010
    “…The developed software can be used to estimate internal loads on a fuselage and to compute the stresses at any point along the length of the fuselage of a given aircraft. …”
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    Proceeding Paper
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