Temperature recovery factors in the transitional and turbulent boundary layer on a 40-degree cone cylinder at Mach number 2.9
By: K. H. Gruenewald.
Contributors: U.S. Naval Ordnance Laboratory, White Oak, Md
Series: U.S. Naval Ordnance Laboratory. Aeroballistic research report -- 168; NAVORD report -- 2742
Publisher: U.S. Naval Ordnance Laboratory
Published: 1953
Place of publication: White Oak, Md
Number of pages: 28
Notes: Bibliographical references: p. 23-24.