LEADER 01973nam  2200517I  450 
001 9910702672103321
005 20141125154953.0
035   $a(CKB)5470000002429466
035   $a(OCoLC)896881922
035   $a(EXLCZ)995470000002429466
100   $a20141125j201402    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPratt & Whitney/Boeing engine validation of noise reduction concepts $efinal report for NASA contract NAS3-97144$hphase 1 /$fDouglas C. Mathews [and six others]
210  1$aEast Hartford, Connecticut :$cUnited Technologies Corporation, Pratt & Whitney ;$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dFebruary 2014.
215   $a1 online resource (vi, 139 pages) $ccolor illustrations
225 1 $aNASA/CR ;$v2014-218088
300   $aTitle from title screen (viewed on Nov. 25, 2014).
300   $a"February 2014."
320   $aIncludes bibliographical references (page 139).
517   $aPratt & Whitney/Boeing engine validation of noise reduction concepts 
606   $aNose inlets$2nasat
606   $aSupersonic flow$2nasat
606   $aImpedance measurement$2nasat
606   $aFlow resistance$2nasat
606   $aNavier-Stokes equation$2nasat
606   $aBoundary layer thickness$2nasat
615  7$aNose inlets.
615  7$aSupersonic flow.
615  7$aImpedance measurement.
615  7$aFlow resistance.
615  7$aNavier-Stokes equation.
615  7$aBoundary layer thickness.
700   $aMathews$b Douglas C.$01386712
712 02$aPratt & Whitney Aircraft Group,
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702672103321
996   $aPratt & Whitney$93538797
997   $aUNINA