LEADER 01595oam  2200469   450 
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035   $a(CKB)5470000002510566
035   $a(OCoLC)1145742747
035   $a(EXLCZ)995470000002510566
100   $a20200323d1934      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of trim angle on the take-off performance of a flying boat /$fby James M. Shoemaker and John R. Dawson
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1934.
215   $a1 online resource (13 pages, 4 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 486
300   $a"January 1934."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aSeaplanes
606   $aSeaplanes$xTakeoff
606   $aSeaplanes$2fast
606   $aSeaplanes$xTakeoff$2fast
615  0$aSeaplanes.
615  0$aSeaplanes$xTakeoff.
615  7$aSeaplanes.
615  7$aSeaplanes$xTakeoff.
700   $aShoemaker$b J. M$g(James Maurice),$01388235
702   $aDawson$b John R.
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   $a9910715346903321
996   $aThe effect of trim angle on the take-off performance of a flying boat$93482519
997   $aUNINA