boundary-layer transition model for the Navier-Stokes computation for a natural-laminar-flow airfoil
By: Nobuhiro Kawai.
Contributors: National Aerospace Laboratory (Japan)
Series: Technical report of the National Aerospace Laboratory -- TR-1038T
Publisher: National Aerospace Laboratory
Published: 1989
Place of publication: Tokyo
Number of pages: 20
Subjects: Boundary layer transition; Laminar flow airfoils
Notes: Includes bibliographical references: p. 19-20.