Further studies on the 21% thick, supercritical NLR airfoil NAE 68-060-21:1
By: M. Khalid and D. J. Jones.
Contributors: Jones, D. J.; National Aeronautical Establishment (Canada)
Publisher: National Aeronautical Establishment
Published: 1986
Place of publication: Ottawa
Number of pages: 27
Subjects: Drag; Reynolds number; Supersonic airfoils
Notes: Bibliographical references: p.8.