Recently, there has been a serious effort to design aircraft that are as small as possible for special, limited-duration missions. These vehicles may carry visual, acoustic, chemical, or biological sensors for such missions as traffic management, hostage situation surveillance, rescue operations, etc.The goal is to develop aircraft systems that weigh less than 90 grams, with a 15-centimeter wingspan. Since it is not possible to meet all of the design requirements of a micro air vehicle with current technology, research is proceeding. This new book reports on the latest research in the area of aerodynamic efficiency of various fixed wing, flapping wing, and rotary wing concepts. It presents the progress made by over 50 active researchers in the field from Canada, Europe, Japan, and the United States. It is the only book of its kind.


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    Titel :

    Euler Solutions for a Finite-Span Flapping Wing


    Beteiligte:


    Erscheinungsdatum :

    2001-01-01


    Format / Umfang :

    23 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Euler Solutions for a Finite-Span Flapping Wing

    Neef, M. F. / Hummel, D. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002


    Thrust Measurements from a Finite-Span Flapping Wing

    Kamalluddien Parker / Julio Soria / Karl Von Ellenrieder | AIAA | 2007


    Wing-span-area-adjustable flapping-wing robot

    WANG JUN / LI FUQIANG | Europäisches Patentamt | 2021

    Freier Zugriff


    Calculation Method for Optimal Circulation Distribution on a Finite Span Flapping Wing

    Harada, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002