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035   $a(CKB)5470000002524934
035   $a(OCoLC)1159597633
035   $a(EXLCZ)995470000002524934
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFlight tests of an airplane showing dependence of the maximum lift coefficient on the test conditions /$fby H.A. Soule? and James A. Hootman
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (12 pages, 3 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 622
300   $a"November 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical reference (page 9).
606   $aAirplanes$xFlight testing
606   $aLift (Aerodynamics)
606   $aAirplanes$xFlight testing$2fast
606   $aLift (Aerodynamics)$2fast
615  0$aAirplanes$xFlight testing.
615  0$aLift (Aerodynamics)
615  7$aAirplanes$xFlight testing.
615  7$aLift (Aerodynamics)
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$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910716724403321
996   $aFlight tests of an airplane showing dependence of the maximum lift coefficient on the test conditions$93483580
997   $aUNINA