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040 a| GPOb| enge| rdae| pnc| GPOd| MvI;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2014-218494;

100 1 a| Ibrahim, Mounir B.,e| author.=| ^A432023;

245 10 a| Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades /c| Mounir Ibrahim and Abhinav Gupta, Vikram Shyam.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| November 2014.;

300 a| 1 online resource (19 pages) :b| color illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM ;v| 2014-218494;

500 a| Title from title screen (viewed Aug. 7, 2015).;

500 a| "November 2014.";

500 a| "Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014.";

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

504 a| Includes bibliographical references (page 19).;

536 a| Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Centerh| WBS 473452.02.03.05.04.02.01;

536 d| E-18962;

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

650 7 a| Turbine blades.2| nasat;

650 7 a| Rotor blades (turbomachinery).2| nasat;

650 7 a| Hole distribution (mechanics).2| nasat;

650 7 a| Hole geometry (mechanics).2| nasat;

700 1 a| Gupta, Abhinav,e| author.=| ^A1271681;

700 1 a| Shyam, Vikram,e| author.=| ^A1419526;

710 2 a| NASA Glenn Research Center,e| issuing body.=| ^A420740;

710 2 a| Fundamental Aeronautics Program (U.S.),e| sponsoring body.=| ^A1093481;

830 0 a| NASA technical memorandumv| 2014-218494.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo57875;

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

596 a| 1;

998 a| 3814224;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3814224-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 9/9/2015x| EDOCUMENTz| JERESOURCE;

Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades / Mounir Ibrahim and Abhinav Gupta, Vikram Shyam.

Author/creator	Ibrahim, Mounir B. author.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, November 2014.
Description	1 online resource (19 pages) : color illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo57875

Other author/creator	Gupta, Abhinav, author.
Other author/creator	Shyam, Vikram, author.
Other author/creator	NASA Glenn Research Center, issuing body.
Other author/creator	Fundamental Aeronautics Program (U.S.), sponsoring body.
Series	NASA/TM ; 2014-218494 NASA technical memorandum 2014-218494. ^A467613
General note	Title from title screen (viewed Aug. 7, 2015).
General note	"November 2014."
General note	"Prepared for the 50th Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Cleveland, Ohio, July 28-30, 2014."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 19).
Funding information	Sponsored by the Fundamental Aeronautics Program at the NASA Glenn Research Center WBS 473452.02.03.05.04.02.01
Funding information	E-18962
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2014-218494

Computational investigation of novel tip leakage mitigation methods for high pressure turbine blades / Mounir Ibrahim and Abhinav Gupta, Vikram Shyam.

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