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037 a| N 90-22566b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:103167;

088 a| AIAA-90-2417;

088 a| E-5539;

100 1 a| Drummond, Colin K.=| ^A435944;

245 12 a| A modeling technique for STOVL ejector and volume dynamics /c| C.K. Drummond and W.S. Barankiewicz ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.;

300 a| 11 p. :b| ill.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 103167;

500 a| Cover title.;

500 a| Shipping list no.: 90-0893-M.;

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 1/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013250%5F1990013250.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 7-8).;

500 a| "AIAA-90-2417.";

500 a| "E-5539"--P. 1.;

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

536 h| 505-62-71;

650 7 a| Aircraft configurations.2| nasat;

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

650 7 a| Mathematical models.2| nasat;

650 7 a| Performance prediction.2| nasat;

650 7 a| Thrust.2| nasat;

650 7 a| V/STOL aircraft.2| nasat;

700 1 a| Barankiewicz, W. S.?| UNAUTHORIZED;

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

830 0 a| NASA technical memorandumv| 103167.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS66379;

949 a| NAS 1.15:103167w| sudoch| joyner32;

596 a| 1;

998 a| 1024875;

999 a| NAS 1.15:103167w| SUDOCc| 1i| MQ1801205d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 2/9/2006x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

A modeling technique for STOVL ejector and volume dynamics / C.K. Drummond and W.S. Barankiewicz ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.

Author/creator	Drummond, Colin K.
Other author	Barankiewicz, W. S.
Other author	United States. National Aeronautics and Space Administration.
Format	Microform
Publication Info	[Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]
Description	11 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS66379
Subjects	Short take-off and landing aircraft--Jet propulsion. --Ejectors. --Mathematical models.

Series	NASA technical memorandum ; 103167 NASA technical memorandum 103167. ^A467613
General note	Cover title.
General note	Shipping list no.: 90-0893-M.
General note	"AIAA-90-2417."
General note	"E-5539"--P. 1.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 7-8).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 1/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013250%5F1990013250.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.
Funding information	505-62-71
Technical rpt number	AIAA-90-2417
Technical rpt number	E-5539
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:103167
Stock number	N 90-22566 NASA

Availability

Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:103167	✔ Available

A modeling technique for STOVL ejector and volume dynamics / C.K. Drummond and W.S. Barankiewicz ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.

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