Local flow conditions, recovery factors and heat-transfer coefficients on the nose of a hemisphere-cylinder at a Mach number of 2.8
By: Irving Korobkin.
Contributors: U.S. Naval Ordnance Laboratory, White Oak, Md
Series: U.S. Naval Ordnance Laboratory. Aeroballistic research report -- 175; NAVORD report -- 2865
Publisher: U.S. Naval Ordnance Laboratory
Published: 1953
Place of publication: White Oak, Md
Number of pages: 13
Notes: Bibliographical references: p. 12.