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040   $aDip.to Matematica$beng
082 0 $a519.5
084   $aAMS 62P30
100 1 $aMarinosci, Antonia$0488474
245 10$aStima della distribuzione statistica del volume di pioggia attraverso le 2-copule di Frank. Tesi di laurea /$claureanda Antonia Marinosci ; relat. Gianfausto Salvadori, Carlo De Michele
260   $aLecce :$bUniversità degli Studi. Facoltà di Scienze. Corso di laurea in Matematica,$ca.a. 2002-03
300   $a36 p. ;$c30 cm
650  4$aApplications of statistics to engineering and industry
700 1 $aSalvadori, Gianfausto
700 1 $aDe Michele, Carlo
907   $a.b13033517$b02-04-14$c13-07-04
912   $a991003164139707536
945   $aLE013 TES 2002/03 MAR3$g1$i2013000146492$lle013$og$pE13.00$q-$rn$s-  $t1$u0$v0$w0$x0$y.i13650361$z13-07-04
996   $aStima della distribuzione statistica del volume di pioggia attraverso le 2-copule di Frank. Tesi di laurea$9287900
997   $aUNISALENTO
998   $ale013$b13-07-04$cm$da  $e-$fita$git $h0$i0

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100   $a20200602d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight /$fby Th. Troller and F. Rokus
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (6 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 735
300   $a"November 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aAerodynamic load
606   $aAirplanes$xWings$xTesting
606   $aFlaps (Airplanes)
606   $aSplit flaps (Airplanes)
606   $aRolling (Aerodynamics)
606   $aYawing (Aerodynamics)
606   $aAerodynamic load$2fast
606   $aAirplanes$xWings$xTesting$2fast
606   $aFlaps (Airplanes)$2fast
606   $aRolling (Aerodynamics)$2fast
606   $aSplit flaps (Airplanes)$2fast
615  0$aAerodynamic load.
615  0$aAirplanes$xWings$xTesting.
615  0$aFlaps (Airplanes)
615  0$aSplit flaps (Airplanes)
615  0$aRolling (Aerodynamics)
615  0$aYawing (Aerodynamics)
615  7$aAerodynamic load.
615  7$aAirplanes$xWings$xTesting.
615  7$aFlaps (Airplanes)
615  7$aRolling (Aerodynamics)
615  7$aSplit flaps (Airplanes)
700   $aTroller$b T.$01414262
702   $aRokus$b Frank G.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910717159703321
996   $aPressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight$93529203
997   $aUNINA