Wind tunnel tests on a 90 degree apex delta wing of variable aspect ratio (sweepback 36.8 degrees). Part I
Subtitle: General stability. Part II : Measurements of downwash and effect of high lift devices
By: J. G. Ross, R. Hills, R. C. Lock and P. Meiklem.
Contributors: Hills, R.; Lock, R. C.; Meiklem, P.; Aeronautical Research Council (Great Britain); Royal Aircraft Establishment (Great Britain)
Series: Aeronautical Research Council. Current paper -- no. 83; Aeronautical Research Council. Report no. Aero 2333; Aeronautical Research Council. Report -- no. Aero 2284
Publisher: Ministry of Supply, Aeronautical Research Council
Published: 1952
Place of publication: London
Number of pages: 19
Notes: Includes bibliographical references.