Research Catalog
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Displaying 1-2 of 2 results
Effect of reduced aft diameter and increased blade number on high-speed counterrotation propeller performance [microform] / Gayle E. Rose, Robert J. Jeracki.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS61130Acoustic test and analysis of a counterrotating prop-fan model [microform] / by: Bernard Magliozzi, Paul Brown, David Parzych.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS61249
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