Determination of the external contour of a body of revolution with a central duct so as to give minimum drag in supersonic flow, with various perimetral conditions imposed upon the missile geometry. Part III
Subtitle: Numerical application
By: Carlo Ferrari.
Contributors: Cornell Aeronautical Laboratory
Publisher: Cornell Aeronautical Laboratory, Inc
Published: 1953
Place of publication: Buffalo
Number of pages: 91
Notes: Report, no. AF-814-A-2.

Bibliography: p. 91.

Contract number: N6ori-119