Curves suitable for families of aerofoils with variable maximum thickness position, nose radius, camber and nose droop
By: L. H. Tanner.
Contributors: Aeronautical Research Council (Great Britain)
Series: Aeronautical Research Council. Current papers -- no. 358
Publisher: Ministry of Supply, Aeronautical Research Council
Published: 1957
Place of publication: London
Number of pages: 15
Notes: Bibliography: p. 15.