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003 OCoLC;

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007 he bmb024bbca;

008 911206s1989 dcua bbt f000 0 eng d;

037 a| N 90-11751b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:4147;

088 a| L-16616;

100 1 a| Riley, Donald R.=| ^A448227;

245 10 a| Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept /c| Donald R. Riley and Gautam H. Shah, Richard E Kuhn.;

246 2 a| Low speed wind tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept;

300 a| 36 p. :b| ill. ;c| 28 cm.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 4147;

500 a| Shipping list no.: 90-0669-M.;

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002435%5F1990002435.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 11).;

500 a| "Performing organization report no.: L-16616"--Technical rept. documentation p.;

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

536 h| 505-61-71-07;

650 0 a| Short take-off and landing aircraft.=| ^A60561;

650 0 a| Vertically rising aircraft.=| ^A60562;

650 0 a| Airplanesx| Control systemsx| Testing.=| ^A313012;

650 7 a| Attitude control.2| nasat;

650 7 a| Fighter aircraft.2| nasat;

650 7 a| Hovering.2| nasat;

650 7 a| Jet flow.2| nasat;

650 7 a| Short takeoff aircraft.2| nasat;

650 7 a| Wind tunnel tests.2| nasat;

700 1 a| Shah, Gautam H.?| UNAUTHORIZED;

700 1 a| Kuhn, Richard E.=| ^A698556;

710 1 a| United States.b| National Aeronautics and Space Administration.b| Scientific and Technical Information Division.=| ^A634451;

830 0 a| NASA technical memorandumv| 4147.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS72303;

949 a| NAS 1.15:4147w| sudoch| joyner32;

596 a| 1;

998 a| 1055286;

999 a| NAS 1.15:4147w| SUDOCc| 1i| MQ1857926d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 9/19/2006x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept / Donald R. Riley and Gautam H. Shah, Richard E Kuhn.

Author/creator	Riley, Donald R.
Other author	Shah, Gautam H.
Other author	Kuhn, Richard E.
Other author	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Format	Microform
Publication Info	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989.
Description	36 p. : ill. ; 28 cm.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS72303
Subjects	Short take-off and landing aircraft. Vertically rising aircraft. Airplanes--Control systems. --Testing.

Variant title	Low speed wind tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept
Series	NASA technical memorandum ; 4147 NASA technical memorandum 4147. ^A467613
General note	Shipping list no.: 90-0669-M.
General note	"Performing organization report no.: L-16616"--Technical rept. documentation p.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 11).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002435%5F1990002435.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.
Funding information	505-61-71-07
Technical rpt number	L-16616
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:4147
Stock number	N 90-11751 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:4147	✔ Available

Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept / Donald R. Riley and Gautam H. Shah, Richard E Kuhn.

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