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001 ocn954593999;

003 OCoLC;

005 20210728172222.0;

006 m o d f ;

007 cr b||||||||||;

008 160803e199611 ohua obt f000 0 eng c;

035 a| (Sirsi) o954593999;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:107374;

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

245 10 a| Predicted turbine heat transfer for a range of test conditions /c| R.J. Boyle and B.L. Lucci.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Lewis Research Center,c| November 1996.;

300 a| 1 online resource (16 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 107374;

500 a| Title from title screen (viewed Aug. 3, 2016).;

500 a| "November 1996"--Report documentation page.;

500 a| "Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996.";

500 a| "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.;

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

504 a| Includes bibliographical references (page 16).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU-505-62-52d| E-10543;

650 7 a| Aerodynamic characteristics.2| nasat;

650 7 a| Heat transfer.2| nasat;

650 7 a| Turbulence models.2| nasat;

650 7 a| Turbine blades.2| nasat;

650 7 a| Wall flow.2| nasat;

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

700 1 a| Lucci, Barbara L.,e| author.=| ^A575197;

710 2 a| Lewis Research Center,e| issuing body.=| ^A367825;

776 08 i| Microfiche version:a| Boyle, Robert J.t| Predicted turbine heat transfer for a range of test conditionsw| (OCoLC)39725937;

830 0 a| NASA technical memorandumv| 107374.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo70711;

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

596 a| 1;

998 a| 5633806;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 5633806-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 5/21/2021x| EDOCUMENTz| JERESOURCE;

Predicted turbine heat transfer for a range of test conditions / R.J. Boyle and B.L. Lucci.

Author/creator	Boyle, Robert J. author.
Other author	Lucci, Barbara L., author.
Other author	Lewis Research Center, issuing body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.
Description	1 online resource (16 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo70711

Series	NASA technical memorandum ; 107374 NASA technical memorandum 107374. ^A467613
General note	Title from title screen (viewed Aug. 3, 2016).
General note	"November 1996"--Report documentation page.
General note	"Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996."
General note	"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 16).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration WU-505-62-52 E-10543
Issued in other form	Microfiche version: Boyle, Robert J. Predicted turbine heat transfer for a range of test conditions
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:107374

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Predicted turbine heat transfer for a range of test conditions / R.J. Boyle and B.L. Lucci.

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