Wind tunnel tests on a 6% two-dimensional aerofoil with 25% chord flap
By: P. E. Turner.
Contributors: Aeronautical Research Laboratories (Australia)
Series: Aeronautical Research Laboratories. Aerodynamics note -- 164
Publisher: Dept. of Supply, Aeronautical Research Laboratories
Published: 1957
Place of publication: Melbourne
Number of pages: 20
Notes: Bibliography: p. 19-20.