LEADER 01849nam  2200505I  450 
001 9910705251403321
005 20141212144352.0
035   $a(CKB)5470000002448853
035   $a(OCoLC)898080688
035   $a(EXLCZ)995470000002448853
100   $a20141212j201306    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aLarge Civil Tiltrotor (LCTR2) interior noise predictions due to turbulent boundary layer excitation /$fFerdinand W. Grosveld
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dJune 2013.
215   $a1 online resource (37 pages) $ccolor illustrations
225 1 $aNASA-CR ;$v2013-218005
300   $aTitle from title screen (viewed Dec. 12, 2014).
300   $a"June 2013."
320   $aIncludes bibliographical references (pages 17-18).
517   $aLarge Civil Tiltrotor 
606   $aAcoustic properties$2nasat
606   $aFinite element method$2nasat
606   $aTurbulent boundary layer$2nasat
606   $aTilt rotor aircraft$2nasat
606   $aSound pressure$2nasat
606   $aFrequency response$2nasat
615  7$aAcoustic properties.
615  7$aFinite element method.
615  7$aTurbulent boundary layer.
615  7$aTilt rotor aircraft.
615  7$aSound pressure.
615  7$aFrequency response.
700   $aGrosveld$b Ferdinand W.$01391334
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705251403321
996   $aLarge Civil Tiltrotor (LCTR2) interior noise predictions due to turbulent boundary layer excitation$93539259
997   $aUNINA