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LEADER 02456nam a2200529Ii 4500

001 ocm46763222;

003 OCoLC;

005 20170725093539.0;

007 he bmb024bbca;

008 010417s1995 dcua bbt f000 0 eng d;

035 a| (Sirsi) o46763222;

037 a| N 97-17022b| NASA;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:112019;

088 a| AIAA 95-1858;

100 1 a| Lin, J. C.,e| author.?| UNAUTHORIZED;

245 10 a| Optimization of an advanced design three-element airfoil at high reynolds numbers /c| J.C. Lin, C.J. Dominik.;

264 1 a| [Washington, D.C.] :b| National Aeronautics and Space Administration,c| [1995];

300 a| 11 pages :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA/TM ;v| 112019;

500 a| "AIAA 13th Applied Aerodynamics Conference, June 19-22, 1995, San Diego, CA.";

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

500 a| "AIAA 95-1858.";

500 a| CRDP Program record.;

650 7 a| Airfoils.2| nasat;

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

650 7 a| High Reynolds number.2| nasat;

650 7 a| Leading edges.2| nasat;

650 7 a| Prediction analysis techniques.2| nasat;

655 7 a| Conference papers and proceedings.2| fast0| (OCoLC)fst01423772;

700 1 a| Dominik, C. J.,e| author.?| UNAUTHORIZED;

710 2 a| American Institute of Aeronautics and Astronautics.=| ^A97214;

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

711 2 a| AIAA Applied Aerodynamics Conferencen| (13th :d| 1995 :c| San Diego, Calif.)?| UNAUTHORIZED;

776 08 i| Print version:t| Optimization of an advanced design three-element airfoil at high reynolds numbersw| (OCoLC)62441720;

776 08 i| Online version:a| Lin, J. C.t| Optimization of an advanced design three-element airfoil at high reynolds numbersw| (OCoLC)990800988;

830 0 a| NASA technical memorandumv| 112019.=| ^A467613;

949 a| NAS 1.15:112019w| sudoch| joyner32;

596 a| 1;

998 a| 4723095;

999 a| NAS 1.15:112019w| SUDOCc| 1i| 4723095-1001l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 7/17/2017x| MICROFORMz| JFEDDOCS;

Optimization of an advanced design three-element airfoil at high reynolds numbers / J.C. Lin, C.J. Dominik.

Author/creator	Lin, J. C. author.
Format	Microform
Publication	[Washington, D.C.] : National Aeronautics and Space Administration, [1995]
Description	11 pages : illustrations.

Other author/creator	Dominik, C. J., author.
Other author/creator	American Institute of Aeronautics and Astronautics.
Other author/creator	United States. National Aeronautics and Space Administration issuing body.
Other author/creator	AIAA Applied Aerodynamics Conference 1995 : San Diego, Calif.) (13th :
Series	NASA/TM ; 112019 NASA technical memorandum 112019. ^A467613
General note	"AIAA 13th Applied Aerodynamics Conference, June 19-22, 1995, San Diego, CA."
General note	"AIAA 95-1858."
General note	CRDP Program record.
Bibliography note	Includes bibliographical references (page 11).
Reproduction note	Microfiche. [Washington, D.C.] : [National Aeronautics and Space Administration], 1997]. 1 microfiche : negative.
Issued in other form	Print version: Optimization of an advanced design three-element airfoil at high reynolds numbers
Issued in other form	Online version: Lin, J. C. Optimization of an advanced design three-element airfoil at high reynolds numbers
Genre/form	Conference papers and proceedings.
Technical rpt number	AIAA 95-1858
GPO item number	0830-D (MF)
Govt. docs number	NAS 1.15:112019
Stock number	N 97-17022 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:112019	✔ Available

Optimization of an advanced design three-element airfoil at high reynolds numbers / J.C. Lin, C.J. Dominik.

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