LEADER 01660nam  2200457   450 
001 9910703627803321
005 20150505160149.0
035   $a(CKB)5470000002433435
035   $a(OCoLC)908402300
035   $a(EXLCZ)995470000002433435
100   $a20150505j201502    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental and computational sonic boom assessment of Boeing N+2 low boom models /$fDonald A. Durston [and five others]
210  1$aMoffett Field, California :$cNational Aeronautics and Space Administration, Ames Research Center,$dFebruary 2015.
215   $a1 online resource (xi, 146 pages) $ccolor illustrations
225 1 $aNASA/TP ;$v2015-218482
300   $aTitle from title screen (viewed May 5, 2015).
300   $a"February 2015."
320   $aIncludes bibliographical references (pages 138-141).
606   $aComputational fluid dynamics$2nasat
606   $aPressure measurement$2nasat
606   $aSonic booms$2nasat
606   $aSupersonic test apparatus$2nasat
606   $aSupersonic wind tunnels$2nasat
615  7$aComputational fluid dynamics.
615  7$aPressure measurement.
615  7$aSonic booms.
615  7$aSupersonic test apparatus.
615  7$aSupersonic wind tunnels.
700   $aDurston$b D. A.$01392553
712 02$aAmes Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703627803321
996   $aExperimental and computational sonic boom assessment of Boeing N+2 low boom models$93447473
997   $aUNINA