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100   $a20170906j199912    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /$fRobert J. Mack
210  1$aHampton, Virginia :$cNational Aeronautics and Space Administration, Langley Research Center,$dDecember 1999.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v1999-209534
300   $a"December 1999."
300   $a"Performing organization: NASA Langley Research Center"--Report documentation page.
320   $aIncludes bibliographical references (pages 13-15).
606   $aAerodynamic characteristics$2nasat
606   $aBody-wing configurations$2nasat
606   $aNacelles$2nasat
606   $aSonic booms$2nasat
606   $aWings$2nasat
606   $aAerodynamic configurations$2nasat
606   $aSupersonic flight$2nasat
606   $aAerodynamic noise$2nasat
606   $aNoise reduction$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAerodynamic characteristics.
615  7$aBody-wing configurations.
615  7$aNacelles.
615  7$aSonic booms.
615  7$aWings.
615  7$aAerodynamic configurations.
615  7$aSupersonic flight.
615  7$aAerodynamic noise.
615  7$aNoise reduction.
615  7$aWind tunnel tests.
700   $aMack$b Robert J.$01408827
712 02$aLangley Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910706143703321
996   $aNacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds$93512804
997   $aUNINA