Tests on an aerofoil with 20 per cent slotted flap and an auxiliary flap in the compressed air tunnel
By: R. Jones and A. H. Bell.
Contributors: Bell, A. H.; Aeronautical Research Committee (Great Britain)
Series: Aeronautical Research Committee. Reports and memoranda -- no. 2109
Publisher: Aeronautical Research Committee
Published: 1939
Place of publication: London
Notes: Bibliography: p. 1.