Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets /
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| Imprint: | [Washington, DC] : National Aeronautics and Space Administration, [1992?] |
|---|---|
| Description: | 1 volume. |
| Language: | English |
| Series: | NASA technical memorandum ; 105935 NASA technical memorandum ; 105935. |
| Subject: | |
| Format: | E-Resource Microform U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/7243881 |
MARC
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| 245 | 0 | 0 | |a Effect of a rotating propeller on the separation angle of attack and distortion in ducted propeller inlets / |c D. R. Boldman, ... [and others]. |
| 264 | 1 | |a [Washington, DC] : |b National Aeronautics and Space Administration, |c [1992?] | |
| 300 | |a 1 volume. | ||
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| 490 | 1 | |a NASA technical memorandum ; |v 105935 | |
| 538 | |a Available via Internet from the NTRS web site. Address as of 07/22/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930007436%5F1993007436.pdf ; current access is available via PURL. | ||
| 650 | 0 | |a Propellers, Aerial. | |
| 650 | 0 | |a Angle of attack (Aerodynamics) | |
| 650 | 7 | |a Angle of attack. |2 nasat | |
| 650 | 7 | |a Flow velocity. |2 nasat | |
| 650 | 7 | |a Inlet flow. |2 nasat | |
| 650 | 7 | |a Separated flow. |2 nasat | |
| 650 | 7 | |a Shrouded propellers. |2 nasat | |
| 650 | 7 | |a Subsonic speed. |2 nasat | |
| 700 | 1 | |a Boldman, Donald R. |0 http://id.loc.gov/authorities/names/no2007055602 |1 http://viaf.org/viaf/2245612 | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://viaf.org/viaf/146202023 | |
| 830 | 0 | |a NASA technical memorandum ; |v 105935. | |
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