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003 OCoLC;

005 20160219102337.0;

006 m o d f ;

007 cr b||||||||||;

008 080513e199705 vaua obt f000 0 eng c;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:4754;

100 1 a| Yeager, William T.,e| author.=| ^A441042;

245 10 a| Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip /c| William T. Yeager, Jr. [and four others].;

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

300 a| 1 online resource (23 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| 4754;

490 1 a| ARL technical report ;v| 1283;

500 a| Title from title screen (viewed on Feb. 19, 2016).;

500 a| "May 1997.";

500 a| "Performing organizations: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center; Joint Research Program Office, Aeroflightdynamics Directorate, U.S. Army Aviation and Troop Command, NASA Langley Research Center"Report documentation page.;

504 a| Includes bibliographical references (page 6).;

500 a| "ATCOM technical report 97-A-006.";

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

650 7 a| Rotary wings.2| nasat;

650 7 a| Vibratory loads.2| nasat;

650 7 a| Transonic wind tunnels.2| nasat;

650 7 a| Paddles.2| nasat;

650 7 a| Rotors.2| nasat;

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| Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tipw| (OCoLC)37002414;

776 08 i| Microfiche version:t| Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tipw| (OCoLC)40711867;

830 0 a| NASA technical memorandumv| 4754.=| ^A467613;

830 0 a| ARL-TR (Aberdeen Proving Ground, Md.) ;v| 1283.=| ^A566074;

856 40 u| https://purl.fdlp.gov/GPO/gpo65467;

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

596 a| 1;

998 a| 4381266;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4381266-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 3/15/2016x| EDOCUMENTz| JERESOURCE;

Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip / William T. Yeager, Jr. [and four others].

Author/creator	Yeager, William T. author.
Other author	Langley Research Center, issuing body.
Other author	United States. National Aeronautics and Space Administration sponsoring body.
Format	Electronic
Publication	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
Description	1 online resource (23 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo65467

Series	NASA technical memorandum ; 4754 ARL technical report ; 1283 NASA technical memorandum 4754. ^A467613 ARL-TR (Aberdeen Proving Ground, Md.) ; 1283. ^A566074
General note	Title from title screen (viewed on Feb. 19, 2016).
General note	"May 1997."
General note	"Performing organizations: Vehicle Technology Center, U.S. Army Research Laboratory, NASA Langley Research Center; Joint Research Program Office, Aeroflightdynamics Directorate, U.S. Army Aviation and Troop Command, NASA Langley Research Center"Report documentation page.
General note	"ATCOM technical report 97-A-006."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 6).
Funding information	Sponsored by the National Aeronautics and Space Administration WU 05-63-36-02 PR A5008 L- 17558 NASA TM-4754 ARL-TR- 1283 ATCOM TR-97-A-006
Issued in other form	Print version: Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
Issued in other form	Microfiche version: Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:4754

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Performance and vibratory loads data from a wind-tunnel test of a model helicopter main-rotor blade with a paddle-type tip / William T. Yeager, Jr. [and four others].

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