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, Jr.
Contributors: Huffman, Jarrett K.; Fox, Charles H.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1988
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Mach number.; Drag (Aerodynamics)
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 2 microfiches.