An experimental investigation by hypersonic flow over blunt nosed cones at a mach number of 5.8.
Contributors: California Institute of Technology
Publisher: California Institute of Technology
Published: 1956
Place of publication: Pasadena, California
Language: eng
Subjects: Aeronautics
Notes: Thesis (AE)--California Institute of Technology, 1956.

Includes bibliographical references. .

Approved for public release, distribution unlimited.