Treatment of two-dimensional jet-flapped wings in incompressible flow, by methods of thin airfoil theory, is extended to case of thin wing of finite aspect ratio which possesses deflected jet sheet of zero thickness emerging with small angular deflection at trailing edge; restriction is imposed that streamlines of jet flow lie in planes perpendicular to wing-span, transverse momentum-transport being thus excluded.
Theory of jet flap in three dimensions
Roy Soc -- Proc
Royal Society -- Proceedings ; 251 , n 1266
1959
19 pages
Article (Journal)
English
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