LEADER 01893nam  2200529 a 450 
001 9910700818203321
005 20111024122806.0
035   $a(CKB)5470000002412838
035   $a(OCoLC)758377228
035   $a(EXLCZ)995470000002412838
100   $a20111024d2011      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMeasured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet$b[electronic resource] /$fDomenic J. Maglieri and Herbert R. Henderson, Ana F. Tinetti
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (65 pages) $cillustrations
225 1 $aNASA/CR ;$v2011-217077
300   $aTitle from title screen (viewed on Oct. 24, 2011).
300   $a"April 2011."
320   $aIncludes bibliographical references (pages 26-28).
606   $aF-104 aircraft$2nasat
606   $aFlow distribution$2nasat
606   $aSonic booms$2nasat
606   $aSupersonic speed$2nasat
606   $aB-70 aircraft$2nasat
606   $aShock waves$2nasat
606   $aWind tunnel tests$2nasat
615  7$aF-104 aircraft.
615  7$aFlow distribution.
615  7$aSonic booms.
615  7$aSupersonic speed.
615  7$aB-70 aircraft.
615  7$aShock waves.
615  7$aWind tunnel tests.
700   $aMaglieri$b Domenic J$01398407
701   $aHenderson$b Herbert R$01414725
701   $aTinetti$b Ana Fiorella$f1962-$01389734
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700818203321
996   $aMeasured sonic boom signatures above and below the XB-70 airplane flying at Mach 1.5 and 37,000 feet$93514798
997   $aUNINA