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003 OCoLC;

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007 he bmb024b|ca;

008 080709s1985 dcu b f000 0 eng d;

037 a| N 85-18957b| NASA;

040 a| GPOc| GPOd| MvI;

049 a| ERE$;

074 a| 0830-D (MF);

074 a| 0830-D (online);

086 0 a| NAS 1.15:86320;

100 1 a| Batina, John T.=| ^A441169;

245 10 a| Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads /c| John T. Batina.;

260 a| Washington, D.C. :b| National Aeronautics and Space Administration, Scientific and Technical Information Branch,c| 1985.;

300 a| 1 v.;

336 a| textb| txt2| rdacontent;

337 a| microformb| h2| rdamedia;

338 a| microficheb| he2| rdacarrier;

490 1 a| NASA technical memorandum ;v| 86320;

530 a| Also available via Internet from the NTRS web site. Address as of 07/08/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850010648%5F1985010648.pdf ; current access is available via PURL.;

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

650 0 a| Aerofoils.=| ^A333143;

650 0 a| Camber (Aerofoils)=| ^A784111;

650 0 a| Unsteady flow (Aerodynamics)=| ^A443874;

650 0 a| Aerodynamics, Transonic.=| ^A186061;

650 0 a| Aerodynamic load.=| ^A613621;

650 7 a| Aerodynamic configurations.2| nasat;

650 7 a| Airfoils.2| nasat;

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

650 7 a| Transonic flow.2| nasat;

710 1 a| United States.b| National Aeronautics and Space Administration.b| Scientific and Technical Information Branch.=| ^A77042;

830 0 a| NASA technical memorandumv| 86320.=| ^A467613;

856 41 u| https://purl.fdlp.gov/GPO/LPS96402;

949 a| NAS 1.15:86320w| sudoch| joyner32;

596 a| 1;

998 a| 1393405;

999 a| NAS 1.15:86320w| SUDOCc| 1i| MQ2578640d| 8/12/2008l| JDOMIm| JOYNERr| Ys| Yt| JDOFMIu| 8/12/2008x| MICROFORMz| JFEDDOCSo| .STAFF. 0;

Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads / John T. Batina.

Author/creator	Batina, John T.
Other author	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Format	Microform
Publication Info	Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Description	1 v.
Supplemental Content	https://purl.fdlp.gov/GPO/LPS96402
Subjects	Aerofoils. Camber (Aerofoils) Unsteady flow (Aerodynamics) Aerodynamics, Transonic. Aerodynamic load.

Series	NASA technical memorandum ; 86320 NASA technical memorandum 86320. ^A467613
General note	GPO Cataloging Record Distribution Program (CRDP).
Other forms	Also available via Internet from the NTRS web site. Address as of 07/08/08: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850010648%5F1985010648.pdf ; current access is available via PURL.
Reproduction note	Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1985. 1 microfiche.
GPO item number	0830-D (MF)
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:86320
Stock number	N 85-18957 NASA

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Library	Location	Call Number	Status	Item Actions
Joyner	Microforms B300	NAS 1.15:86320	✔ Available

Effects of airfoil shape, thickness, camber, and angle of attack on calculated transonic unsteady airloads / John T. Batina.

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