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Exercise on Hess-Smith panel method for 2D airfoils, 4 digit series

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  • 1

    2014 5

    &

    1. NACA 4321/4406 E.N. Jacobs, K.E. Ward, & R.M. Pinkerton, NACA (1933) Report No. 460, p.23:

    ( . .., http://digital.library.unt.edu/ark:/67531/metadc65698/m1/25/ ) . c/4

    1 : () -

    C

    , MC NACA 4321 NACA 4406

    panel.m.

    ()

    NACA (. 1) Glauert

    (. 4 ).

    :

    ()

    4 = , 0 , 4 8 . -

    .

    2 : ()

    ,

    .

    () (., .., 2 3). () C

    , MC NACA 4 (. 1)

    Glauert, .

    : 1. : http://arion.naval.ntua.gr/~banthy/ 2. Milne-Thomson, 1973, Theoretical Aerodynamics, Dover Books ( Googlebooks) 3. http://commons.wikimedia.org/wiki/Category:NACA_4-digit_Airfoils

    & & 9, 157 73 , .: (210) 7721061, 7721138 Fax : (210) 7721397 E-mail: [email protected]

    NATIONAL TECHNICAL UNIVERSITY OF ATHENS DEPT. OF NAVAL ARCHITECTURE & MARINE ENGINEERING SECTION OF SHIP & MARINE HYDRODYNAMICS LABORATORY OF SHIP & MARINE HYDRODYNAMICS Heroon Polytechniou 9, 157 73 Zografos, Athens, GREECE Tel.: (++30-210) 7721061, 7721138 Fax: (++30-210) 7721397 E-mail: [email protected]

  • 2

    2. / http://commons.wikimedia.org/wiki/File:Examples_of_Airfoils.svg

    3. / von Mises Milne-Thomson, Theoretical Aerodynamics (p.131-134)