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001 ocn793599684;

003 OCoLC;

005 20120515091415.0;

006 m d f ;

007 cr c||||||||||;

008 120515s2011 vaua obt f000 0 eng d;

040 a| GPOc| GPOd| MvI;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2011-217316;

245 00 a| Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight :b| preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel /c| Anthony Neal Watkins ... [et al.].;

260 a| Hampton, Va. :b| National Aeronautics and Space Administration, Langley Research Center,c| [2011];

300 a| 1 online resource (18 p.) :b| col. ill.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2011-217316;

500 a| Title from title screen (viewed on May 15, 2012).;

500 a| "December 2011.";

500 a| GPO Cataloging Record Distribution Program (CRDP).;

504 a| Includes bibliographical references (p. 17-18).;

536 d| L-20095;

536 h| 877868.02.07.07.06.03.01;

650 7 a| Pressure measurement.2| nasat;

650 7 a| Pressure sensitive paints.2| nasat;

650 7 a| Flow distribution.2| nasat;

650 7 a| Flight simulation.2| nasat;

650 7 a| Pressure sensors.2| nasat;

650 7 a| Horizontal flight.2| nasat;

650 7 a| Blade tips.2| nasat;

700 1 a| Watkins, Anthony Neal.?| UNAUTHORIZED;

710 2 a| Langley Research Center.=| ^A192893;

830 0 a| NASA technical memorandumv| 217316.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo22695;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 3074361;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3074361-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 6/21/2012x| EDOCUMENTz| JERESOURCE;

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 / Anthony Neal Watkins ... [et al.].

Other author	Watkins, Anthony Neal.
Other author	Langley Research Center.
Format	Electronic
Publication Info	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Description	1 online resource (18 p.) : col. ill.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo22695

Series	NASA/TM ; 2011-217316 NASA technical memorandum 217316. ^A467613
General note	Title from title screen (viewed on May 15, 2012).
General note	"December 2011."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 17-18).
Funding information	L-20095
Funding information	877868.02.07.07.06.03.01
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2011-217316

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 / Anthony Neal Watkins ... [et al.].

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