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LEADER 02734cam 2200589Ia 4500

001 ocm42889963;

003 OCoLC;

005 20160802103506.0;

007 he bmb024bbca;

008 991126s1996 cau b f000 0 eng d;

035 a| (Sirsi) o42889963;

037 a| 19970003552b| NASA;

043 a| n-us---;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:104326;

100 1 a| Holzman, Jon K.=| ^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| [Holzman, Jon K.].;

300 a| 1 unnumbered page ;c| 28 cm;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

500 a| Author and title from microfiche header.;

500 a| Shipping list no.: 98-0799-M.;

500 a| "Abstract.";

500 a| CRDP Project record.;

650 0 a| Aircraft exhaust emissionsz| United States.=| ^A219066;

650 0 a| Jet enginesz| United States.=| ^A426470;

650 0 a| F-16 (Jet fighter plane)=| ^A141431;

650 7 a| Aircraft exhaust emissions.2| fast0| (OCoLC)fst00802815;

650 7 a| F-16 (Jet fighter plane)2| fast0| (OCoLC)fst00919298;

650 7 a| Jet engines.2| fast0| (OCoLC)fst00982398;

651 7 a| United States.2| fast0| (OCoLC)fst01204155?| UNAUTHORIZED;

650 7 a| Jet engines.2| nasat;

650 7 a| Exhaust gases.2| nasat;

650 7 a| Mass flow rate.2| nasat;

650 7 a| Mach number.2| nasat;

650 7 a| Flight tests.2| nasat;

650 7 a| Flow characteristics.2| nasat;

650 7 a| Pressure measurement.2| nasat;

650 7 a| Velocity measurement.2| nasat;

650 7 a| Temperature measurement.2| nasat;

710 2 a| NASA Dryden Flight Research Center.=| ^A420724;

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| Online 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 testsw| (OCoLC)703662716;

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

596 a| 1;

998 a| 750236;

999 a| NAS 1.15:104326w| SUDOCc| 1i| MQ1370623d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 6/14/2000x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

[Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests] / [Holzman, Jon K.].

Author/creator	Holzman, Jon K.
Other author	NASA Dryden Flight Research Center.
Format	Microform
Publication Info	[Edwards, Calif.] : [NASA Dryden Flight Research Center] ; [Springfield, Va.] : [National Technical Information Service, distributor], [1996]
Description	1 unnumbered page ; 28 cm
Subjects	Aircraft exhaust emissions--United States. Jet engines--United States. F-16 (Jet fighter plane)

Series	NASA technical memorandum 104326. ^A467613
General note	Author and title from microfiche header.
General note	Shipping list no.: 98-0799-M.
General note	"Abstract."
General note	CRDP Project record.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997]. 1 microfiche : negative. (NASA-TM ; 104326).
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	Online 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 (MF)
Govt. docs number	NAS 1.15:104326
Stock number	19970003552 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:104326	✔ Available

[Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests] / [Holzman, Jon K.].

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