Imai, I. (1944) Two-Dimensional Aero-Foil Theory for Compressible Fluids. Rep. Aero. Research Institute, Tokyo Imperial University, No. 294.

has been cited by the following article:

• TITLE: An Iteration Method to Solve the Boundary Layer Flow past a Flat Plate

  AUTHORS: Ken-ichi Kusukawa, Shigeaki Suwa, Takeo R. M. Nakagawa

  KEYWORDS: Boundary Layer Flow; Mathematical Analysis; Iteration Method; Approximate Solution; Navier-Stokes Equation

  JOURNAL NAME: Journal of Applied Mathematics and Physics, Vol.2 No.4, March 13, 2014

  ABSTRACT: An iteration method similar to the thin-wing-expansion method for the compressible flow has been proposed to solve the boundary layer flow past a flat plate. Using such an iteration, the first step of which is Oseen’s approximation, the boundary layer past a flat plate is studied. As proceeding from the first approximation to the second and third approximations, it is realized that our solution approaches to a well known Howarth’s bench mark one gradually. Hence, it is concluded that the usefulness of the present method has been confirmed.