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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Reynolds Numbers


    Beteiligte:


    Erscheinungsdatum :

    2001-01-01


    Format / Umfang :

    27 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Aerodynamic Characteristics of Low Aspect Ratio Wings at Low Reynolds Numbers

    Torres, G. E. / Mueller, T. J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2002



    Effect of Aspect Ratio on Aerodynamic Characteristics of Rectangular Wings at Low Reynolds Numbers

    Mizoguchl, M. / Itoh, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012


    Aerodynamic Damping Derivatives of Low Aspect Ratio Wings at Low Reynolds Numbers

    Shields, M.C. / Mohseni, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013