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040 a| GPOb| enge| rdae| pnc| GPOd| MvI;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:4760;

100 1 a| Wilkie, W. Keats,e| author.?| UNAUTHORIZED;

245 10 a| Rotating shake test and modal analysis of a model helicopter rotor blade /c| W. Keats Wilkie, Paul H. Mirick, and Chester W. Langston.;

264 1 a| Hampton, Virginia :b| National Aeronautics and Space Administration, Langley Research Center,c| June 1997.;

300 a| 1 online resource (15 pages.) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 4760;

500 a| Title from title screen (viewed on Feb. 18, 2016).;

500 a| "June 1997.";

500 a| "Performing organizations: NASA Langley Research Center, Hampton, VA [and] Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton, VA"--Report documentation page.;

504 a| Includes bibliographical references (page 15).;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU 505-63-36-02d| A5008d| L-17352;

500 a| "ARL technical report 1389.";

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

650 7 a| Rotary wings.2| nasat;

650 7 a| Helicopters.2| nasat;

650 7 a| Aeroelasticity.2| nasat;

650 7 a| Hovering.2| nasat;

650 7 a| Torsion.2| nasat;

700 1 a| Mirick, Paul H.,e| author.=| ^A1230200;

700 1 a| Langston, Chester W.,e| author.?| UNAUTHORIZED;

710 2 a| Vehicle Technology Center (U.S. Army Research Laboratory)=| ^A430270;

710 2 a| Langley Research Center,e| issuing body.=| ^A192893;

710 1 a| United States.b| National Aeronautics and Space Administratione| sponsoring body.=| ^A5437;

776 08 i| Print version:t| Rotating shake test and modal analysis of a model helicopter rotor bladew| (OCoLC)437089421;

776 08 i| Microfiche version:a| Wilkie, W. Keats.t| Rotating shake test and modal analysis of a model helicopter rotor bladew| (OCoLC)41975252;

830 0 a| NASA technical memorandumv| 4760.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo65480;

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

596 a| 1;

998 a| 4381928;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4381928-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 3/15/2016x| EDOCUMENTz| JERESOURCE;

Rotating shake test and modal analysis of a model helicopter rotor blade / W. Keats Wilkie, Paul H. Mirick, and Chester W. Langston.

Author/creator	Wilkie, W. Keats author.
Format	Electronic
Publication	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, June 1997.
Description	1 online resource (15 pages.) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo65480

Other author/creator	Mirick, Paul H., author.
Other author/creator	Langston, Chester W., author.
Other author/creator	Vehicle Technology Center (U.S. Army Research Laboratory)
Other author/creator	Langley Research Center, issuing body.
Other author/creator	United States. National Aeronautics and Space Administration sponsoring body.
Series	NASA technical memorandum ; 4760 NASA technical memorandum 4760. ^A467613
General note	Title from title screen (viewed on Feb. 18, 2016).
General note	"June 1997."
General note	"Performing organizations: NASA Langley Research Center, Hampton, VA [and] Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center, Hampton, VA"--Report documentation page.
General note	"ARL technical report 1389."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 15).
Funding information	Sponsored by the National Aeronautics and Space Administration WU 505-63-36-02 A5008 L-17352
Issued in other form	Print version: Rotating shake test and modal analysis of a model helicopter rotor blade
Issued in other form	Microfiche version: Wilkie, W. Keats. Rotating shake test and modal analysis of a model helicopter rotor blade
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:4760

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Rotating shake test and modal analysis of a model helicopter rotor blade / W. Keats Wilkie, Paul H. Mirick, and Chester W. Langston.

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