Hypersonic tunnel no. 4 results IX: the development of a water-cooled strain-gage balance (including sting effects) and its application to a study of normal force and pitching moments of a cone and cone-cylinder at Mach numbers 5 to 8
By: L. L. Liccini.
Contributors: U.S. Naval Ordnance Laboratory (White Oak, Md)
Series: NAVORD. Aeroballistic research report -- 347; NAVORD report -- 4334
Publisher: U.S. Naval Ordnance Laboratory
Published: 1956
Place of publication: White Oak, Md
Number of pages: 11
Notes: Bibliography: p. 10-11.