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001 ocn703662716;

003 OCoLC;

005 20210407142117.0;

006 m o d f ;

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

008 110224e199611 caua obt f000 0 eng d;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:104326;

100 1 a| Holzman, Jon K.,e| author.=| ^A1296373;

245 10 a| Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests /c| Jon K. Holzman, Lannie D. Webb, and Frank W. Burcham, Jr.;

264 1 a| Edwards, California. :b| National Aeronautics and Space Administration, Dryden Flight Research Center,c| November 1996.;

300 a| 1 online resource (iv, 26 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| 104326;

500 a| Title from title screen (viewed April 5, 2016).;

500 a| "November 1996.";

500 a| "Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.;

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

504 a| Includes bibliographical references (page 26).;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU 505-68-10d| H-2122;

650 7 a| Acoustic measurement.2| nasat;

650 7 a| Aircraft noise.2| nasat;

650 7 a| Engine noise.2| nasat;

650 7 a| Exhaust gases.2| nasat;

650 7 a| Jet engines.2| nasat;

700 1 a| Webb, Lannie D.,e| author.=| ^A426191;

700 1 a| Burcham, Frank W.,e| author.=| ^A424635;

710 2 a| NASA Dryden Flight Research Centere| issuing body.=| ^A420724;

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

776 08 i| Print version:t| Flight and static exhaust flow properties of an f110-ge-129 engine in an f-16xl airplane during acoustic tests ... nasa-tm-104326 ... mar. 31w| (OCoLC)213887209;

776 08 i| Microfiche version:a| Holzman, Jon K.t| [Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests]w| (OCoLC)42889963;

830 0 a| NASA technical memorandumv| 104326.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo66654;

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

596 a| 1;

998 a| 4407180;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4407180-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 5/27/2016x| EDOCUMENTz| JERESOURCE;

Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests / Jon K. Holzman, Lannie D. Webb, and Frank W. Burcham, Jr.

Author/creator	Holzman, Jon K. author.
Format	Electronic
Publication	Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, November 1996.
Description	1 online resource (iv, 26 pages) : illustrations
Supplemental Content	https://purl.fdlp.gov/GPO/gpo66654

Other author/creator	Webb, Lannie D., author.
Other author/creator	Burcham, Frank W., author.
Other author/creator	NASA Dryden Flight Research Center issuing body.
Other author/creator	United States. National Aeronautics and Space Administration sponsoring body.
Series	NASA technical memorandum ; 104326 NASA technical memorandum 104326. ^A467613
General note	Title from title screen (viewed April 5, 2016).
General note	"November 1996."
General note	"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 26).
Funding information	Sponsored by the National Aeronautics and Space Administration WU 505-68-10 H-2122
Issued in other form	Print version: Flight and static exhaust flow properties of an f110-ge-129 engine in an f-16xl airplane during acoustic tests ... nasa-tm-104326 ... mar. 31
Issued in other form	Microfiche version: Holzman, Jon K. [Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests]
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:104326

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Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests / Jon K. Holzman, Lannie D. Webb, and Frank W. Burcham, Jr.

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