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LEADER 01595cam a2200421Ka 4500

001 ocn162126535;

003 OCoLC;

005 20141208173845.0;

008 070802s1986 ohu b f000 0 eng d;

035 a| (Sirsi) o162126535;

035 a| (OCoLC)162126535;

040 a| GPOc| GPOd| MvId| UtOrBLW;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:87298;

100 1 a| Hwang, Danny P.=| ^A1436819;

245 12 a| A numerical analysis applied to high angle of attack three-dimensional inlets /c| Danny P. Hwang.;

260 a| [Cleveland, Ohio] :b| [National Aeronautics and Space Administration, Lewis Research Center],c| [1986];

300 a| 1 volume.;

336 a| text2| rdacontent;

337 a| microform2| rdamedia;

338 a| microfiche2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 87298;

650 0 a| Angle of attack (Aerodynamics)=| ^A593563;

650 0 a| Fluid dynamics.=| ^A18739;

650 7 a| Angle of attack.2| nasat;

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

650 7 a| Engine inlets.2| nasat;

650 7 a| Inlet flow.2| nasat;

650 7 a| Panel method (fluid dynamics)2| nasat;

650 7 a| Potential flow.2| nasat;

650 7 a| Separated flow.2| nasat;

710 2 a| Lewis Research Center.=| ^A367825;

830 0 a| NASA technical memorandumv| 87298.=| ^A467613;

596 a| 1;

998 a| 1094357;

999 a| NAS 1.15:87298w| SUDOCc| 1i| MQ1938368l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 9/19/2007x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

A numerical analysis applied to high angle of attack three-dimensional inlets / Danny P. Hwang.

Author/creator	Hwang, Danny P.
Other author	Lewis Research Center.
Format	Book
Publication Info	[Cleveland, Ohio] : [National Aeronautics and Space Administration, Lewis Research Center], [1986]
Description	1 volume.
Subjects	Angle of attack (Aerodynamics) Fluid dynamics.

Series	NASA technical memorandum ; 87298 NASA technical memorandum 87298. ^A467613
Reproduction note	Joyner- Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.
GPO item number	0830-D (MF)
Govt. docs number	NAS 1.15:87298

Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:87298	✔ Available

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