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LEADER 02859nam a2200589 i 4500

001 on1001438248;

003 OCoLC;

005 20171102094809.0;

006 m o d f ;

007 cr bn|||||||||;

008 170821e199901 ohua obt f000 0 eng c;

035 a| (Sirsi) o1001438248;

042 a| pcc;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:208501;

100 1 a| Rigby, D. L.q| (David Lester),d| 1963-e| author.=| ^A1128133;

245 10 a| Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn /c| David L. Rigby.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Lewis Research Center,c| January 1999.;

300 a| 1 online resource (12 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 1999-208501;

500 a| "January 1999.";

500 a| "Prepared for the 43rd Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998.";

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

500 a| CRDP Program record.;

504 a| Includes bibliographical references (pages 11-12).;

513 a| Technical memorandum.;

536 a| Sponsored by the National Aeronautics and Space Administrationd| WU-523-26-13-00d| E-11300;

588 a| Description based on online resource; title from PDF title page (NASA, viewed Aug. 21, 2017).;

650 7 a| Reynolds averaging.2| nasat;

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

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

650 7 a| Turbine blades.2| nasat;

650 7 a| Cooling systems.2| nasat;

650 7 a| Mass transfer.2| nasat;

650 7 a| Heat transfer.2| nasat;

650 7 a| K-omega turbulence model.2| nasat;

650 7 a| Engine coolants.2| nasat;

650 7 a| Computational grids.2| nasat;

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

776 08 i| Print version:t| Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turnw| (OCoLC)213890627;

776 08 i| Microfiche version:a| Rigby, D. L. (David Lester), 1963-t| Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turnw| (OCoLC)42042478;

830 0 a| NASA technical memorandumv| 1999-208501.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo83981;

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

596 a| 1;

998 a| 4751399;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4751399-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 9/14/2017x| EDOCUMENTz| JERESOURCE;

Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn / David L. Rigby.

Author/creator	Rigby, D. L., 1963- author.
Other author	Lewis Research Center, issuing body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, January 1999.
Description	1 online resource (12 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo83981

Series	NASA/TM ; 1999-208501 NASA technical memorandum 1999-208501. ^A467613
General note	"January 1999."
General note	"Prepared for the 43rd Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998."
General note	"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
General note	CRDP Program record.
Bibliography note	Includes bibliographical references (pages 11-12).
Report note	Technical memorandum.
Funding information	Sponsored by the National Aeronautics and Space Administration WU-523-26-13-00 E-11300
Source of description	Description based on online resource; title from PDF title page (NASA, viewed Aug. 21, 2017).
Issued in other form	Print version: Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn
Issued in other form	Microfiche version: Rigby, D. L. (David Lester), 1963- Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:208501

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Prediction of heat and mass transfer in a rotating ribbed coolant passage with a 180 degree turn / David L. Rigby.

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