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100   $a20111115j198012    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /$fGeorge C. Ashby, Jr
210  1$a[Washington, D.C.] :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dDecember 1980.
215   $a1 online resource (31 pages) $cillustrations
225 1 $aNASA technical paper ;$v1787
300   $aTitle from title screen (viewed on Aug. 23, 2016).
300   $a"December 1980."
300   $a"Performing Organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (page 9).
606   $aBlunt bodies$2nasat
606   $aFar fields$2nasat
606   $aFinite difference theory$2nasat
606   $aSonic booms$2nasat
606   $aStatic pressure$2nasat
606   $aAerodynamics, Supersonic$2fast
606   $aSonic boom$2fast
615  7$aBlunt bodies.
615  7$aFar fields.
615  7$aFinite difference theory.
615  7$aSonic booms.
615  7$aStatic pressure.
615  7$aAerodynamics, Supersonic.
615  7$aSonic boom.
700   $aAshby$b George C.$0196768
712 02$aLangley Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707438803321
996   $aA study of the sonic-boom characteristics of a blunt body at a Mach number of 6$93434677
997   $aUNINA