Supersonic drag calculations for a cylindrical shell wing of semi-circular cross-section combined with a central body of revolution
By: Beverly J. Beane and B. M. Ryan.
Contributors: Ryan, B. M.; Douglas Aircraft Company
Series: Douglas Aircraft Company. Report -- no. SM-22627
Publisher: Douglas Aircraft Company
Published: 1956
Place of publication: Santa Monica, Calif
Number of pages: 33
Notes: Bibliography: p. 32-33.