Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance
By: Gayle E. Rose, Robert J. Jeracki.
Contributors: Jeracki, Robert J.; Lewis Research Center.
Series: NASA technical memorandum -- 102077.
Publisher: National Aeronautics and Space Administration, Lewis Research Center; For sale by the National Technical Information Service
Published: 1989
Place of publication: [Cleveland, Ohio]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft engines.; Counterrotation.; Diameters.; Propeller blades.
Notes: Also available via Internet from the NASA Technical Report Server web site. Address as of 6/23/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900004036%5F1990004036.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche.