Higher-order approximations in interactive airfoil calculations
By: David Walter Zingg.
Series: UTIAS report -- no.326
Publisher: Institute for Aerospace Studies
Published: 1988
Place of publication: [Downsview, Ont.]
Subjects: Airfoils; Boundary layers; Computational fluid dynamics; Incompressible flow; Interactive methods; Pressure gradients; Subsonic flow
Notes: Bibliographical references: p.[103-114].