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001 ocn703664188;

003 OCoLC;

005 20171102094743.0;

006 m o d f ;

007 cr bn|||||||||;

008 110224e199902 caua obt f000 0 eng c;

035 a| (Sirsi) o703664188;

042 a| dca| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:206572;

100 1 a| Steenken, William G.,e| author.=| ^A455154;

245 10 a| Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft /c| W.G. Steenken [and three others].;

264 1 a| Edwards, California :b| National Aeronautics and Space Administration, Dryden Flight Research Center,c| February 1999.;

300 a| 1 online resource (vii, 191 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 1999-206572;

500 a| "February 1999.";

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

500 a| CRDP Program record.;

504 a| Includes bibliographical references (page 34).;

513 a| Technical memorandum.;

536 a| Prepared for NASA Dryden Flight Research Centerd| WU 529-31-04-00-37-00-F18d| H-2327;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Aug. 18, 2017).;

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

650 7 a| Aerodynamic stability.2| nasat;

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

650 7 a| Compressors.2| nasat;

650 7 a| Control surfaces.2| nasat;

650 7 a| Flight control.2| nasat;

650 7 a| Research vehicles.2| nasat;

650 7 a| Rotors.2| nasat;

650 7 a| Subsonic speed.2| nasat;

710 2 a| Dryden Flight Research Facilitye| issuing body.=| ^A424598;

776 08 i| Microfiche version:t| Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraftw| (OCoLC)41964667;

830 0 a| NASA technical memorandumv| 1999-206572.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo83895;

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

596 a| 1;

998 a| 4750978;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4750978-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 9/14/2017x| EDOCUMENTz| JERESOURCE;

Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft / W.G. Steenken [and three others].

Author/creator	Steenken, William G. author.
Other author	Dryden Flight Research Facility issuing body.
Format	Electronic
Publication	Edwards, California : National Aeronautics and Space Administration, Dryden Flight Research Center, February 1999.
Description	1 online resource (vii, 191 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo83895

Series	NASA/TM ; 1999-206572 NASA technical memorandum 1999-206572. ^A467613
General note	"February 1999."
General note	"Performing organization: NASA Dryden Flight Research Center"--Report documentation page.
General note	CRDP Program record.
Bibliography note	Includes bibliographical references (page 34).
Report note	Technical memorandum.
Funding information	Prepared for NASA Dryden Flight Research Center WU 529-31-04-00-37-00-F18 H-2327
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Aug. 18, 2017).
Issued in other form	Microfiche version: Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:206572

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Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft / W.G. Steenken [and three others].

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