Tests in the Royal Aircraft Establishment 10-ft x 7-ft high-speed tunnel on 50-deg swept-back wings. Part I. Three of 7.5 per cent thickness. Part II. One of 7.5 per cent thickness with stall fences and leading-edge chord extension
By: A. B. Haines and C. W. Rhodes.
Contributors: Rhodes, C. W.; Aeronautical Research Council (Great Britain)
Series: Aeronautical Research Council. Reports and memoranda -- no. 3043
Publisher: Ministry of Supply, Aeronautical Research Council
Published: 1954
Place of publication: London
Number of pages: 84
Notes: Cover date: 1957.

Bibliography: p. 52.