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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$aExperimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models /$fSusan E. Cliff [and four others]
210  1$aMoffett Field, CA :$cNational Aeronautics and Space Administration, Ames Research Center,$dJanuary 2015.
215   $a1 online resource (258 pages) $ccolor illustrations
225 1 $aNASA/TP ;$v2015-218483
300   $aTitle from title screen (viewed Sept. 16, 2015).
300   $a"January 2015."
320   $aIncludes bibliographical references (pages 62-66).
606   $aSonic booms$2nasat
606   $aSupersonic aircraft$2nasat
606   $aAircraft configurations$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aSupersonic test apparatus$2nasat
615  7$aSonic booms.
615  7$aSupersonic aircraft.
615  7$aAircraft configurations.
615  7$aComputational fluid dynamics.
615  7$aSupersonic test apparatus.
700   $aCliff$b Susan E.$01396907
712 02$aAmes Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703964503321
996   $aExperimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models$93457827
997   $aUNINA

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200 1 $aFormal and transcendental logic$fEdmund Husserl$gtraduzione di Dorion Cairns
210   $aNetherlands$cMartinus Nijhoff$d1978
215   $a340 p.$d24 cm
610 0 $aLogica
610 0 $aLogica formale
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700  1$aHusserl,$bEdmund$035554
801  2$aIT$bUNINA$gRICA$2UNIMARC
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952   $a10 DO 130 TA$bDONOTAMBURRINI130/23$fDINEL
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