ergasiabanthy2014
DESCRIPTION
Exercise on Hess-Smith panel method for 2D airfoils, 4 digit seriesTRANSCRIPT
-
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)