Examples of calculation of minimum supersonic drag due to lift by solution of two-dimensional potential problem: elliptical-planform wings and an approximate delta-planform wing
By: M. E. Graham.
Contributors: Douglas Aircraft Company
Series: Douglas Aircraft Company. Report -- no. SM-22754
Publisher: Douglas Aircraft Company
Published: 1957
Place of publication: Santa Monica, Calif
Number of pages: 15
Notes: Bibliography: p. 12.