Calculation of optimum lift distribution for the sonic-edge diamond planform wing from spanwise moments obtained from the corresponding artificial singularity distribution
By: Beverly J. Beane.
Contributors: Douglas Aircraft Company
Series: Douglas Aircraft Company. Report -- no. SM-23017
Publisher: Douglas Aircraft Company
Published: 1957
Place of publication: Santa Monica, Calif
Number of pages: 14
Notes: Bibliography: p. 14.