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    Titel :

    Low Reynolds Number High-Lift Airfoil Design for HALE Concept UAV



    Kongress:

    25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA



    Erscheinungsdatum :

    2006-01-01


    Format / Umfang :

    AIAA Paper 2006-3462


    Anmerkungen:

    Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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