Section characteristics up to Mach 1.01 of a 6% aerofoil having a 25% chord flap at 0 degrees and 4 degrees
By: A. S. Bennett.
Contributors: Aeronautical Research Laboratories (Australia)
Series: Aeronautical Research Laboratories.  Aerodynamics note -- 179
Publisher: Aeronautical Research Laboratories
Published: 1960
Place of publication: Melbourne
Number of pages: 11