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

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2015-218841;

100 1 a| Davis, David O.,e| author.=| ^A1408370;

245 10 a| CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction /c| David O. Davis.;

246 3 a| Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| September 2015.;

300 a| 1 online resource (13 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| 2015-218841;

500 a| Title from title screen (viewed on Feb. 2, 2016).;

500 a| "September 2015.";

500 a| "Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015;

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

504 a| Includes bibliographical references (page 13).;

536 d| AJK2015-0634;

650 7 a| Boundary layers.2| nasat;

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

650 7 a| Shock wave interaction.2| nasat;

650 7 a| Flow measurement.2| nasat;

650 7 a| Turbulent flow.2| nasat;

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

830 0 a| NASA technical memorandumv| 2015-218841.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo64648;

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

596 a| 1;

998 a| 4381692;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 4381692-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 3/15/2016x| EDOCUMENTz| JERESOURCE;

CFD validation experiment of a Mach 2.5 axisymmetric shock-wave/boundary-layer interaction / David O. Davis.

Author/creator	Davis, David O. author.
Other author	NASA Glenn Research Center, issuing body.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2015.
Description	1 online resource (13 pages) : color illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo64648

Variant title	Computational fluid dynamics validation experiment of a Mach 2.5 axisymmetric shock wave boundary layer interaction
Series	NASA/TM ; 2015-218841 NASA technical memorandum 2015-218841. ^A467613
General note	Title from title screen (viewed on Feb. 2, 2016).
General note	"September 2015."
General note	"Prepared for the Joint Fluids Engineering Conference 2015 cosponsored by ASME, JSME, and KSME, Seoul, Korea, July 26-31, 2015
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 13).
Funding information	AJK2015-0634
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2015-218841

Library	Location	Call Number	Status	Item Actions
	Electronic Resources	Access Content Online	✔ Available

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