LEADER 01751nam  2200481I  450 
001 9910705749003321
005 20170623064941.0
035   $a(CKB)5470000002452917
035   $a(OCoLC)990800988
035   $a(EXLCZ)995470000002452917
100   $a20170623d1995      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aOptimization of an advanced design three-element airfoil at high Reynolds numbers /$fJ.C. Lin, C.J. Dominik
210  1$a[Washington, D.C.]:$cNational Aeronautics and Space Administration,$d[1995].
215   $a1 online resource (11 pages) $cillustrations
225 1 $aNASA-TM ;$v112019
300   $a"AIAA 13th Applied Aerodynamics Conference, June 19-22, 1995, San Diego, CA."
300   $a"AIAA 95-1858."
320   $aIncludes bibliographical references (page 11).
606   $aAirfoils$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aHigh Reynolds number$2nasat
606   $aLeading edges$2nasat
606   $aPrediction analysis techniques$2nasat
615  7$aAirfoils.
615  7$aComputational fluid dynamics.
615  7$aHigh Reynolds number.
615  7$aLeading edges.
615  7$aPrediction analysis techniques.
700   $aLin$b J.-C$g(Jiun-Chuan),$0612234
702   $aDominik$b C. J.
712 02$aAmerican Institute of Aeronautics and Astronautics.
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705749003321
996   $aOptimization of an advanced design three-element airfoil at high Reynolds numbers$93468132
997   $aUNINA