Description 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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    Title :

    Adaptive, Unstructured Meshes for Solving the Navier-Stokes Equations for Low-Chord-Reynolds-Number Flows


    Contributors:


    Publication date :

    2001-01-01




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English



    Adaptive, Unstructured Meshes for Solving the Navier-Stokes Equations for Low-Chord-Reynolds-Number Flows

    Monttinen, J. T. / Shortridge, R. R. / Latek, B. S. et al. | British Library Conference Proceedings | 2002




    Automatic Generation of Unstructured Meshes for Navier Stokes Flows

    Peraire, J. / Morgan, K. / AIAA | British Library Conference Proceedings | 1998