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
By: Carlo Ferrari.
Contributors: Cornell Aeronautical Laboratory
Series: Cornell Aeronautical Laboratory. Report -- no. AF-814-A-1
Publisher: Cornell Aeronautical Laboratory, Inc
Published: 1953
Place of publication: Buffalo
Number of pages: 66
Notes: Bibliographical references: p. 66.

Contract number: N-6ori-119