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003 OCoLC;

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006 m o d f ;

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

008 110224e199706 caua ot f000 0 eng d;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:104327;

100 1 a| Yuhas, Andrew J.,e| author.?| UNAUTHORIZED;

245 10 a| F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack /c| Andrew J. Yuhas [and three others].;

264 1 a| Edwards, California. :b| National Aeronautics and Space Administration, Dryden Flight Research Center,c| June 1997.;

300 a| 1 online resource (18 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| 104327;

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

500 a| "June 1997.";

500 a| "Under NASA Dryden Flight Research Center contract NAS 3-26617.";

500 a| "Performing organization: Analytical Services & Materials, Inc., Edwards, California [and] General Electric Aircraft Engines, Cincinnati, Ohio"--Report documentation page.;

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

536 a| Sponsored by the National Aeronautics and Space Administrationb| NAS 3-26617d| WU 505-68-30d| H-2146;

650 7 a| Aircraft maneuvers.2| nasat;

650 7 a| Angle of attack.2| nasat;

650 7 a| Distortion.2| nasat;

650 7 a| F-18 aircraft.2| nasat;

650 7 a| Inlet flow.2| nasat;

710 2 a| Analytical Services & Materials, Inc.=| ^A1293749;

710 2 a| General Electric Company.b| Aircraft Engine Business Group.=| ^A1033564;

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| Microfiche version:t| F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attackw| (OCoLC)40617095;

830 0 a| NASA technical memorandumv| 104327.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo66655;

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

596 a| 1;

998 a| 4407178;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4407178-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 5/27/2016x| EDOCUMENTz| JERESOURCE;

F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack / Andrew J. Yuhas [and three others].

Author/creator	Yuhas, Andrew J. author.
Format	Electronic
Publication	Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, June 1997.
Description	1 online resource (18 pages) : illustrations
Supplemental Content	https://purl.fdlp.gov/GPO/gpo66655

Other author/creator	Analytical Services & Materials, Inc.
Other author/creator	General Electric Company. Aircraft Engine Business Group.
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 ; 104327 NASA technical memorandum 104327. ^A467613
General note	Title from title screen (viewed April 5, 2016).
General note	"June 1997."
General note	"Under NASA Dryden Flight Research Center contract NAS 3-26617."
General note	"Performing organization: Analytical Services & Materials, Inc., Edwards, California [and] General Electric Aircraft Engines, Cincinnati, Ohio"--Report documentation page.
General note	GPO Cataloging Record Distribution Program (CRDP).
Funding information	Sponsored by the National Aeronautics and Space Administration NAS 3-26617 WU 505-68-30 H-2146
Issued in other form	Microfiche version: F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:104327

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F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack / Andrew J. Yuhas [and three others].

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