LEADER 01986oam  2200565 a 450 
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035   $a(CKB)5470000002420205
035   $a(OCoLC)785219635
035   $a(EXLCZ)995470000002420205
100   $a20120410d1985      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 13$aAn airfoil flutter model suspension system to accommodate large static transonic airloads$b[electronic resource] /$fWilmer H. Reed, III
210  1$aNewport News, VA :$cDEI-Tech, Inc. ;$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[1985]
215   $a1 online resource (36 pages) $cillustrations
225 1 $aNASA contractor report ;$v177998
225 1 $aNASA-CR-177998
300   $aTitle from title screen (viewed Apr. 10, 2012).
300   $a"October 1985."
320   $aIncludes bibliographical references (pages 18-19).
606   $aAirfoils$2nasat
606   $aBlowdown wind tunnels$2nasat
606   $aFlutter analysis$2nasat
606   $aPressure distribution$2nasat
606   $aStatic pressure$2nasat
606   $aSupercritical airfoils$2nasat
606   $aTransonic wind tunnels$2nasat
606   $aTwo dimensional flow$2nasat
615  7$aAirfoils.
615  7$aBlowdown wind tunnels.
615  7$aFlutter analysis.
615  7$aPressure distribution.
615  7$aStatic pressure.
615  7$aSupercritical airfoils.
615  7$aTransonic wind tunnels.
615  7$aTwo dimensional flow.
700   $aReed$b Wilmer H$01390193
712 02$aDEI-Tech, Inc.
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910701788903321
996   $aAn airfoil flutter model suspension system to accommodate large static transonic airloads$93442728
997   $aUNINA