LEADER 02117oam  2200589   450 
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035   $a(CKB)5470000002524828
035   $a(OCoLC)1159597612
035   $a(EXLCZ)995470000002524828
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails$hI$iBasic loading condition /$fby Oscar Seidman and A.I. Neihouse
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (13 pages, 17 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 608
300   $a"August 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 12-13).
517 3 $aBasic loading condition
606   $aSpin (Aerodynamics)
606   $aAirplanes$xWings
606   $aAirplanes$xTail surfaces
606   $aWind tunnel testing
606   $aAirplanes$xTail surfaces$2fast
606   $aAirplanes$xWings$2fast
606   $aSpin (Aerodynamics)$2fast
606   $aWind tunnel testing$2fast
615  0$aSpin (Aerodynamics)
615  0$aAirplanes$xWings.
615  0$aAirplanes$xTail surfaces.
615  0$aWind tunnel testing.
615  7$aAirplanes$xTail surfaces.
615  7$aAirplanes$xWings.
615  7$aSpin (Aerodynamics)
615  7$aWind tunnel testing.
700   $aSeidman$b Oscar$01405963
702   $aNeihouse$b A. I.
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   $a9910716734903321
996   $aFree-spinning wind-tunnel tests of a low-wing monoplane with systematic changes in wings and tails$93483584
997   $aUNINA