LEADER 01927oam  2200493Ia 450 
001 9910701902203321
005 20120806144759.0
035   $a(CKB)5470000002423101
035   $a(OCoLC)804877134
035   $a(EXLCZ)995470000002423101
100   $a20120806d1985      ua             0
101 0 $aeng
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAnalysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed$b[electronic resource] /$fby Arthur F. Smith
210  1$aWindsor Locks, Conn. :$cHamilton Standard Division, United Technologies Corporation ;$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center,$d[1985]
215   $a1 online resource (x, 101/102 pages) $cillustrations
225 1 $aNASA CR ;$v175026
300   $aTitle from title screen (viewed on Aug. 6, 2012).
300   $a"December, 1985."
320   $aIncludes bibliographical references (page 29/30).
606   $aAerodynamic stability$2nasat
606   $aDynamic response$2nasat
606   $aDynamic structural analysis$2nasat
606   $aEvaluation$2nasat
606   $aProp-fan technology$2nasat
606   $aTurboprop engines$2nasat
615  7$aAerodynamic stability.
615  7$aDynamic response.
615  7$aDynamic structural analysis.
615  7$aEvaluation.
615  7$aProp-fan technology.
615  7$aTurboprop engines.
700   $aSmith$b Arthur F$0130914
712 02$aLewis Research Center.
712 02$aUnited Technologies Corporation.$bHamilton Standard Division.
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910701902203321
996   $aAnalysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed$93495404
997   $aUNINA