LEADER 01899nam  2200505I  450 
001 9910702418703321
005 20170113122529.0
035   $a(CKB)5470000002427985
035   $a(OCoLC)884519933
035   $a(EXLCZ)995470000002427985
100   $a20140724d2013      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAeroservoelastic testing of free flying wind tunnel models /$fRobert C. Scott [and four others]
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$d2013.
215   $a1 online resource (2 volumes) $ccolor illustrations
225 1 $aNASA/TP ;$v2013-218051
300   $aTitle from title screen (viewed on July 24, 2014).
300   $a"October 2013."
320   $aIncludes bibliographical references.
327   $apt 1. A sidewall supported semispan model tested for gust load alleviation and flutter suppression. -- pt 2. A centerline supported fullspan model tested for gust load alleviation.
606   $aAeroservoelasticity$2nasat
606   $aFlaps (control surfaces)$2nasat
606   $aGust loads$2nasat
606   $aSemispan models$2nasat
606   $aTransonic wind tunnels$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAeroservoelasticity.
615  7$aFlaps (control surfaces)
615  7$aGust loads.
615  7$aSemispan models.
615  7$aTransonic wind tunnels.
615  7$aWind tunnel tests.
700   $aScott$b Robert C.$06557
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702418703321
996   $aAeroservoelastic testing of free flying wind tunnel models$93550082
997   $aUNINA