LEADER 01686nam  2200481I  450 
001 9910702488503321
005 20130114103408.0
035   $a(CKB)5470000002427280
035   $a(OCoLC)824145508
035   $a(EXLCZ)995470000002427280
100   $a20130114d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aApplication of the semi-empirical force-limiting approach for the CoNNeCT SCAN Testbed /$fLucas D. Staab [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d2012.
215   $a1 online resource (iii, 30 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217627
300   $aTitle from title screen (viewed on Jan. 14, 2013).
300   $a"September 2012."
320   $aIncludes bibliographical references (page 30).
606   $aImpedance$2nasat
606   $aVibration tests$2nasat
606   $aDynamic structural analysis$2nasat
606   $aRandom vibration$2nasat
606   $aMathematical models$2nasat
606   $aDynamic response$2nasat
615  7$aImpedance.
615  7$aVibration tests.
615  7$aDynamic structural analysis.
615  7$aRandom vibration.
615  7$aMathematical models.
615  7$aDynamic response.
700   $aStaab$b Lucas D.$01396813
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702488503321
996   $aApplication of the semi-empirical force-limiting approach for the CoNNeCT SCAN Testbed$93457575
997   $aUNINA