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008 970709s1971    de            ||| | eng  
020   $a354005541X
035   $ab10824042-39ule_inst
035   $aLE01309642$9ExL
040   $aDip.to Matematica$beng
082 0 $a511.3
084   $aAMS 03F
100 1 $aScarpellini, Bruno$050397
245 10$aProof theory and intuitionistic systems /$cBruno Scarpellini
260   $aBerlin ; New York :$bSpringer-Verlag,$c1971
300   $avii, 290, [1] p. ;$c24 cm
490 0 $aLecture notes in mathematics,$x0075-8434 ;$v212
500   $aBibliography: p. [291]
650  0$aIntuitionistic mathematics
650  0$aProof theory
907   $a.b10824042$b23-02-17$c28-06-02
912   $a991001269069707536
945   $aLE013 03F SCA11 (1971)$g1$i2013000089010$lle013$o-$pE0.00$q-$rl$s-  $t0$u0$v0$w0$x0$y.i10931703$z28-06-02
996   $aProof theory and intuitionistic systems$981444
997   $aUNISALENTO
998   $ale013$b01-01-97$cm$da  $e-$feng$gde $h0$i1

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100   $a20200623d1938      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design /$fby H.A. Soule? and James A. Hootman
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1938.
215   $a1 online resource (12 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 653
300   $a"June 1938."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 12).
606   $aAilerons
606   $aAirplanes$xFlight testing
606   $aAeronautics$xResearch
606   $aAeronautics$xResearch$2fast
606   $aAilerons$2fast
606   $aAirplanes$xFlight testing$2fast
615  0$aAilerons.
615  0$aAirplanes$xFlight testing.
615  0$aAeronautics$xResearch.
615  7$aAeronautics$xResearch.
615  7$aAilerons.
615  7$aAirplanes$xFlight testing.
700   $aSoule$b Hartley A$g(Hartley Akin),$f1904-1988,$01399820
702   $aHootman$b James A.
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   $a9910716869403321
996   $aA flight investigation of the reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design$93521784
997   $aUNINA