Three-Dimensional Flow Separation of A Plane, Incompressible, Laminar Boundary Layer Caused by A Half-Delta Wing on A Flat Plate.
Contributors: Shen, P.S.; Jones, D.J.
Series: Canada Nrc Aeronautical Report lr -- 471; Publication (National Research Council Canada) -- 9634
Publisher: s.n
Published: 1967
Place of publication: S.l
Language: eng
Notes: 1