Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
By: Sheryll Goecke Powers, Jarrett K. Huffman and Charles H. Fox.
Contributors: Fox, Charles H.; Huffman, Jarrett K.; Dryden Flight Research Facility
Publisher: Dryden Flight Research Facility
Published: 1986
Place of publication: Edwards, Cal
Number of pages: 139
Subjects: Blunt bodies; Bodies of revolution; Drag reduction; Trapped vortexes; Turbulent flow
Notes: Bibliographical references: p.22-23.