An approximate method for calculating the hypersonic flow around circular cones at zero angle of attack, including real gas effects
By: John W. Brook.
Contributors: Grumman Aircraft Engineering Corporation. Research Dept.
Series: Grumman Aircraft Engineering Corporation.  Research Dept. report -- RE-132
Publisher: Grumman Aircraft Engineering Corporation, Research Dept.
Published: 1960
Place of publication: Bethpage, N.Y
Number of pages: 26
Notes: Bibliographic references: p. 16.