Tests on a 16% Handley-Page aerofoil with 20% slotted flap in the compressed air tunnel
By: D. H. Williams, A. H. Bell and E. Smyth.
Contributors: Bell, A. H.; Smyth, E.; Aeronautical Research Committee (Great Britain)
Series: Aeronautical Research Committee. Reports and memoranda -- no. 1854
Publisher: Aeronautical Research Committee
Published: 1938
Place of publication: London
Number of pages: 18