LEADER 01806nam  2200481   450 
001 9910711552903321
005 20181107101614.0
035   $a(CKB)5470000002484522
035   $a(OCoLC)1061504789
035   $a(EXLCZ)995470000002484522
100   $a20181107j201810    ua             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design /$fDavid J. Friedlander, Christopher M. Heath, and Raymond S. Castner
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2018.
215   $a1 online resource (55 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2018-219967
300   $a"October 2018."
320   $aIncludes bibliographical references (page 55).
517   $aNumerical simulations of a Quiet SuperSonic Technology 
606   $aComputational fluid dynamics$2nasat
606   $aSupersonic aircraft$2nasat
606   $aReynolds averaging$2nasat
606   $aGrid refinement (mathematics)$2nasat
606   $aComputerized simulation$2nasat
615  7$aComputational fluid dynamics.
615  7$aSupersonic aircraft.
615  7$aReynolds averaging.
615  7$aGrid refinement (mathematics)
615  7$aComputerized simulation.
700   $aFriedlander$b David J.$01398592
702   $aHeath$b Christopher M.
702   $aCastner$b Raymond S.
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910711552903321
996   $aNumerical simulations of a Quiet SuperSonic Technology (QueSST) aircraft preliminary design$93512241
997   $aUNINA