Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel /
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| Imprint: | Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] |
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| Description: | 1 online resource (18 p.) : col. ill. |
| Language: | English |
| Series: | NASA/TM ; 2011-217316 NASA technical memorandum ; 217316. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/8832487 |