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200 00$aQuerela geometrica, or, Geometry's complaint of the injuries lately received from Mr. Thomas VVhite in his late tract entituled, Tutela geometrica$b[electronic resource] $ein the end you have some places at large out of Mr. White's Tutela, and Gulden's Centrobaryca, reprinted, and faithfully translated into English
210   $aLondon $cPrinted by R.W.$d1660
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300   $aReproduction of original in British Library.
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606   $aGeometry$vEarly works to 1800
615  0$aGeometry
701  2$aWhite$b Thomas$f1593-1676.$0793401
701  2$aGuldin$b Paul$f1577-1643.$01011470
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997   $aUNISA

LEADER 02196oam  2200613   450 
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100   $a20200519d1939      ua             0
101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing /$fby Rufus O. House
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (5 pages, 5 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 719
300   $a"July 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aAirplanes$xModels$xWings
606   $aSlotted flaps (Airplanes)
606   $aFlaps (Airplanes)
606   $aAerodynamics
606   $aWind tunnel testing
606   $aAerodynamics$2fast
606   $aAirplanes$xModels$xWings$2fast
606   $aFlaps (Airplanes)$2fast
606   $aSlotted flaps (Airplanes)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xModels$xWings.
615  0$aSlotted flaps (Airplanes)
615  0$aFlaps (Airplanes)
615  0$aAerodynamics.
615  0$aWind tunnel testing.
615  7$aAerodynamics.
615  7$aAirplanes$xModels$xWings.
615  7$aFlaps (Airplanes)
615  7$aSlotted flaps (Airplanes)
615  7$aWind tunnel testing.
700   $aHouse$b R. O.$01392490
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
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906   $aBOOK
912   $a9910717166803321
996   $aThe effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing$93529206
997   $aUNINA