NOL Hypersonic Tunnel no. 4 results VI
Subtitle: experimental and theoretical investigation of the boundary layer and heat transfer characteristics of a cooled hypersonic wedge nozzle at a Mach number of 5.5
By: E. M. Winkler and Jerome Persh.
Contributors: Persh, Jerome.; U.S. Naval Ordnance Laboratory, White Oak, Md
Series: U.S. Naval Ordnance Laboratory. Aeroballistic research report -- 245; NAVORD report -- 3757
Publisher: U.S. Naval Ordnance Laboratory
Published: 1954
Place of publication: White Oak, Md
Number of pages: 11
Notes: Bibliographical references: p. 11.