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001 9910705749303321
005 20170622150731.0
035   $a(CKB)5470000002452914
035   $a(OCoLC)990788328
035   $a(EXLCZ)995470000002452914
100   $a20170622d1995      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /$fKenneth M. Jones, Robert T. Biedron, Mark Whitlock
210  1$a[Washington, D.C.]:$cNational Aeronautics and Space Administration,$d[1995].
215   $a1 online resource (25 pages) $cillustrations
225 1 $aNASA-TM ;$v112005
300   $a"13th Applied Aerodynamics Conference June 19-22, 1995, San Diego, California."
300   $a"AIAA 95-1855."
320   $aIncludes bibliographical references (page 12).
606   $aAerodynamic configurations$2nasat
606   $aAirfoils$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aReynolds number$2nasat
606   $aWing flaps$2nasat
615  7$aAerodynamic configurations.
615  7$aAirfoils.
615  7$aComputational fluid dynamics.
615  7$aNavier-Stokes equation.
615  7$aReynolds number.
615  7$aWing flaps.
700   $aJones$b Kenneth M.$01408986
702   $aBiedron$b Robert T.
702   $aWhitlock$b Mark
712 02$aAmerican Institute of Aeronautics and Astronautics.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910705749303321
996   $aApplication of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques$93514416
997   $aUNINA