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006 m d f ;

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

008 110613s2010 ohua obt f000 0 eng d;

040 a| GPOc| GPOd| MvI;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2010-216897;

100 1 a| Connolly, Joseph W.=| ^A1043320;

245 10 a| Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds /c| Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010.;

260 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| [2010];

300 a| 1 online resource (19 p.) :b| ill. (col.);

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2010-216897;

500 a| Title from title screen (viewed on June 13, 2011).;

500 a| "October 2010.";

504 a| Includes bibliographical references (p. 18-19).;

500 a| "AIAA-2010-7068.";

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

536 h| WBS 984754.02.07.03.20.02;

650 7 a| Supersonic flight.2| nasat;

650 7 a| Control systems design.2| nasat;

650 7 a| Supersonic transports.2| nasat;

650 7 a| Specifications.2| nasat;

650 7 a| Supersonic inlets.2| nasat;

650 7 a| Dynamic models.2| nasat;

650 7 a| Loops.2| nasat;

650 7 a| Feedback control.2| nasat;

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

650 7 a| Flow distribution.2| nasat;

650 7 a| Computational fluid dynamics.2| nasat;

700 1 a| Kopasakis, George.=| ^A1043318;

710 2 a| NASA Glenn Research Center.=| ^A420740;

711 2 a| AIAA/ASME/SAE/ASEE Joint Propulsion Conferencen| (46th :d| 2010 :c| Nashville, Tenn.)?| UNAUTHORIZED;

830 0 a| NASA technical memorandumv| 216897.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo8439;

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

596 a| 1;

998 a| 2508327;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 2508327-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 7/7/2011x| EDOCUMENTz| JERESOURCE;

Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds / Joseph W. Connolly and George Kopasakis ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010.

Author/creator	Connolly, Joseph W.
Other author	Kopasakis, George.
Other author	NASA Glenn Research Center.
Other author	AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2010 : Nashville, Tenn.)
Format	Electronic
Publication Info	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010]
Description	1 online resource (19 p.) : ill. (col.)
Supplemental Content	https://purl.fdlp.gov/GPO/gpo8439

Series	NASA/TM ; 2010-216897 NASA technical memorandum 216897. ^A467613
General note	Title from title screen (viewed on June 13, 2011).
General note	"October 2010."
General note	"AIAA-2010-7068."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 18-19).
Funding information	WBS 984754.02.07.03.20.02
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2010-216897

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