LEADER 01615nam  2200445I  450 
001 9910702349803321
005 20130115152519.0
035   $a(CKB)5470000002426661
035   $a(OCoLC)824454877
035   $a(EXLCZ)995470000002426661
100   $a20130115d2012      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExperimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration /$fFloyd J. Wilcox, Jr. [and five others]
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2012]
215   $a1 online resource (130 pages) $cillustrations
225 1 $a[NASA technical memorandum] ;$vNASA/TM-2012-217598
300   $aTitle from title screen (viewed Jan. 15, 2013).
300   $a"August 2012."
320   $aIncludes bibliographical references (pages 9-10).
606   $aSonic booms$2nasat
606   $aWind tunnel tests$2nasat
606   $aSupersonic speed$2nasat
606   $aAngle of attack$2nasat
615  7$aSonic booms.
615  7$aWind tunnel tests.
615  7$aSupersonic speed.
615  7$aAngle of attack.
700   $aWilcox$b Floyd J$g(Floyd Jay),$01386305
712 02$aLangley Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702349803321
996   $aExperimental sonic boom measurements on a Mach 1.6 cruise low-boom configuration$93435169
997   $aUNINA