The calculation of interference drag between wing lift and fuselage thickness at supersonic speeds
By: E. W. Graham and R. M. Licher.
Contributors: Licher, R. M.; Douglas Aircraft Corporation
Series: Douglas Aircraft Corporation. Report -- no. SM-23446
Publisher: Douglas Aircraft Corporation
Published: 1959
Place of publication: Santa Monica, Calif
Number of pages: 23
Notes: Bibliography: p. 22-23.