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LEADER 01727cam a2200433Ka 4500

001 ocn243639582;

003 OCoLC;

005 20141212005046.0;

007 he bmb024bbca;

008 080813s1983 cau b f000 0 eng d;

035 a| (Sirsi) o243639582;

035 a| (OCoLC)243639582;

040 a| GPOc| GPOd| EREd| UtOrBLW;

049 a| ERE$;

074 a| 0830-D (MF);

086 0 a| NAS 1.15:84319;

100 1 a| Geissler, Wolfgang,c| Dr.-Ing.=| ^A785673;

245 10 a| Unsteady laminar boundary-layer calculations on oscillating configurations including backflow.n| Part II,p| Airfoil in high-amplitude pitching motion - dynamic stall /c| W. Geissler.;

246 3 a| Airfoil in high-amplitude ptiching motion--dynamic stall;

260 a| Moffett Field, Calif. :b| National Aeronautics and Space Administration, Ames Research Center,c| [1983];

300 a| 1 volume.;

336 a| text2| rdacontent;

337 a| microform2| rdamedia;

338 a| microfiche2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 84319;

650 0 a| Boundary layerx| Analysis.=| ^A39412;

650 0 a| Helicoptersx| Aerodynamics.=| ^A165402;

650 7 a| Amplitudes.2| nasat;

650 7 a| Boundary layers.2| nasat;

650 7 a| Finite difference theory.2| nasat;

650 7 a| Flat plates.2| nasat;

650 7 a| Incompressible flow.2| nasat;

710 2 a| Ames Research Center.=| ^A101004;

830 0 a| NASA technical memorandumv| 84319.=| ^A467613;

994 a| C0b| ERE;

596 a| 1;

998 a| 1397143;

999 a| NAS 1.15:84319w| SUDOCc| 1i| MQ2605009l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 9/11/2008x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Unsteady laminar boundary-layer calculations on oscillating configurations including backflow. / W. Geissler.

Author/creator	Geissler, Wolfgang
Other author	Ames Research Center.
Format	Microform
Publication Info	Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
Description	1 volume.
Subjects	Boundary layer--Analysis. Helicopters--Aerodynamics.

Variant title	Airfoil in high-amplitude ptiching motion--dynamic stall
Series	NASA technical memorandum ; 84319 NASA technical memorandum 84319. ^A467613
Reproduction note	Joyner- Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1984. 1 microfiche.
GPO item number	0830-D (MF)
Govt. docs number	NAS 1.15:84319

Availability

Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:84319	✔ Available

Unsteady laminar boundary-layer calculations on oscillating configurations including backflow. / W. Geissler.

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