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001 ocm25311495;

003 OCoLC;

005 20060215122132.0;

007 he bmb024bbca;

008 920221s1990 dcua bbt f000 0 eng c;

037 a| N 90-21300b| NASA;

042 a| pcc;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:102496;

088 a| E-5219;

100 1 a| Boyle, Robert J.=| ^A431828;

245 10 a| Navier-Stokes analysis of turbine blade heat transfer /c| R.J. Boyle ; prepared for the 35th International Gas Turbine and Aeroengine Congress and Exposition sponsored by the American Society of Mechanical Engineers, Brussels, Belgium, June 11-14, 1990.;

246 2 a| Navier Stokes analysis of turbine blade heat transfer;

300 a| 19 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| 102496;

500 a| Cover title.;

500 a| Shipping list no.: 90-0858-M.;

530 a| Also available via Internet from the NASA Technical Report Server web site. Address as of 2/13/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011984%5F1990011984.pdf; current access available via PURL.;

504 a| Includes bibliographical references (p. 8-9).;

500 a| "Performing organization report no.: E-5219"--Technical rept. documentation p.;

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

536 h| 505-62-21;

650 0 a| Turbinesx| Blades.=| ^A599371;

650 0 a| Heatx| Transmission.=| ^A18327;

650 7 a| Aerothermodynamics.2| nasat;

650 7 a| Heat transfer.2| nasat;

650 7 a| Navier-Stokes equation.2| nasat;

650 7 a| Reynolds number.2| nasat;

650 7 a| Separated flow.2| nasat;

650 7 a| Turbine blades.2| nasat;

650 7 a| Vanes.2| nasat;

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

830 0 a| NASA technical memorandumv| 102496.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS66714;

949 a| NAS 1.15:102496w| sudoch| joyner32;

596 a| 1;

998 a| 1028617;

999 a| NAS 1.15:102496w| SUDOCc| 1i| MQ1806130d| 8/7/2007l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 3/14/2006x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Navier-Stokes analysis of turbine blade heat transfer / R.J. Boyle ; prepared for the 35th International Gas Turbine and Aeroengine Congress and Exposition sponsored by the American Society of Mechanical Engineers, Brussels, Belgium, June 11-14, 1990.

Author/creator	Boyle, Robert J.
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	19 p. : ill.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS66714
Subjects	Turbines--Blades. Heat--Transmission.

Variant title	Navier Stokes analysis of turbine blade heat transfer
Series	NASA technical memorandum ; 102496 NASA technical memorandum 102496. ^A467613
General note	Cover title.
General note	Shipping list no.: 90-0858-M.
General note	"Performing organization report no.: E-5219"--Technical rept. documentation p.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (p. 8-9).
Other forms	Also available via Internet from the NASA Technical Report Server web site. Address as of 2/13/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011984%5F1990011984.pdf; current access available via PURL.
Reproduction note	Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990] 1 microfiche : negative.
Funding information	505-62-21
Technical rpt number	E-5219
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:102496
Stock number	N 90-21300 NASA

Navier-Stokes analysis of turbine blade heat transfer / R.J. Boyle ; prepared for the 35th International Gas Turbine and Aeroengine Congress and Exposition sponsored by the American Society of Mechanical Engineers, Brussels, Belgium, June 11-14, 1990.

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