LEADER 00859nam0-22002891i-450-
001 990003142430403321
035   $a000314243
035   $aFED01000314243
035   $a(Aleph)000314243FED01
035   $a000314243
100   $a20000920d--------km-y0itay50------ba
101 0 $aita
102   $aIT
200 1 $aNominal Rigidities in a Mail Order Company$eEstimation of the Probability of Price Adjustment$fSilvia Bertarelli
225 1 $aCollana del Dipartimento di scienze economiche, Università di Bologna$v349
610 0 $aPrezzi$aItalia
676   $aF/1.411
676   $aI/2.120
702  1$aBertarelli,$bSilvia
801  0$aIT$bUNINA$gRICA$2UNIMARC
901   $aBK
912   $a990003142430403321
952   $aPaper$fSES
959   $aSES
996   $aNominal Rigidities in a Mail Order Company$9455829
997   $aUNINA
DB    $aING01

LEADER 01133nam0-2200385---450 
001 990005599510203316
005 20190403124923.0
035   $a000559951
035   $aUSA01000559951
035   $a(ALEPH)000559951USA01
035   $a000559951
100   $a19981214d1996----|||y0itaa50------ba
101   $afre
102   $afr
105   $a0 00|||
200 1 $aFenelon et l'amour de Dieu$fpar Denis Leduc-Fayette
210   $aParis$cPUF$d1996
215   $a126 p.$d18 cm.
225 2 $aPhilosophies$fcollection dirigée par Françoise Balibar ...[et al.]$v66
410  0$12001$aPhilosophies$v66
606   $aFenelon, François de Salignac : de la Mothe$2F
620   $dPARIS
676   $a231.6
700  1$aLEDUC-FAYETTE,$bDenis$0614863
801  0$aIT$bSA$c20111219
912   $a990005599510203316
950  0$aDipar.to di Filosofia - Salerno$dDFCC 231.6 LED$e2595 FIL
951   $aCC 231.6 LED$b2595 FIL
959   $aBK
969   $aFIL
979   $c20121027$lUSA01$h1525
979   $c20121027$lUSA01$h1614
996   $aFenelon et l'amour de Dieu$91133107
997   $aUNISA
NUM   $aSA0003111

LEADER 02005oam  2200553   450 
001 9910713823203321
005 20240125000127.0
035   $a(CKB)5470000002505423
035   $a(OCoLC)1104148289
035   $a(EXLCZ)995470000002505423
100   $a20190610d1933      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes /$fby Robert Sanders
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1933.
215   $a1 online resource (9 pages, 3 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 477
300   $a"November 1933."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 7).
606   $aWind tunnel testing
606   $aAirplanes$xWings$xTesting
606   $aTailless airplanes
606   $aAspect ratio (Aerofoils)
606   $aAirplanes, Tailless$2fast
606   $aAirplanes$xWings$xTesting$2fast
606   $aAspect ratio (Aerofoils)$2fast
615  0$aWind tunnel testing.
615  0$aAirplanes$xWings$xTesting.
615  0$aTailless airplanes.
615  0$aAspect ratio (Aerofoils)
615  7$aAirplanes, Tailless.
615  7$aAirplanes$xWings$xTesting.
615  7$aAspect ratio (Aerofoils)
700   $aSanders$b Robert$f1908-1992,$01421142
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713823203321
996   $aAerodynamic tests of a low aspect ratio tapered wing with an auxiliary airfoil for use on tailless airplanes$93541652
997   $aUNINA