An approach to the design of airfoils with high lift to drag ratios
By: David Walter Zingg.
Contributors: University of Toronto. Institute for Aerospace Studies.
Series: UTIAS technical note -- no.245
Publisher: Institute for Aerospace Studies
Published: 1983
Place of publication: [Downsview, Ont.]
Number of pages: 59
Subjects: Airfoils; Lift drag ratio; Panel method
Notes: Bibliographical references: p. 39-41.