LEADER 01831nam  2200481 a 450 
001 9910700812003321
005 20110927104033.0
035   $a(CKB)5470000002412901
035   $a(OCoLC)754813291
035   $a(EXLCZ)995470000002412901
100   $a20110927d2011      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aConical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry$b[electronic resource] /$fGregory C. Herring and James F. Meyers
210  1$aHampton, Va. :$cNational Aeronautics and Space Administration, Langley Research Center,$d[2011]
215   $a1 online resource (29 pages) $cillustrations (some color)
225 1 $aNASA/TM ;$v2011-217052
300   $aTitle from title screen (viewed on Sept. 27, 2011).
300   $a"February 2011."
320   $aIncludes bibliographical references (pages 16-18).
517 3 $aConical shock strength determination on low sonic boom aircraft model by doppler global velocimetry
606   $aVelocity measurement$2nasat
606   $aSonic booms$2nasat
606   $aFlow characteristics$2nasat
606   $aSupersonic speed$2nasat
606   $aOblique shock waves$2nasat
615  7$aVelocity measurement.
615  7$aSonic booms.
615  7$aFlow characteristics.
615  7$aSupersonic speed.
615  7$aOblique shock waves.
700   $aHerring$b Gregory C$01394410
701   $aMeyers$b James F$01405402
712 02$aLangley Research Center.
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910700812003321
996   $aConical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry$93504828
997   $aUNINA