LEADER 01959oam  2200565   450 
001 9910716799203321
005 20210730141315.0
035   $a(CKB)5470000002524179
035   $a(OCoLC)1159597596
035   $a(EXLCZ)995470000002524179
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel tests of a Clark Y wing with "Maxwell" leading-edge slots /$fby William E. Gauvain
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (6 pages, 9 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 598
300   $a'"April 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 6).
606   $aAirplanes$xWings
606   $aLeading edges (Aerodynamics)
606   $aTrailing edge flaps
606   $aWind tunnel testing
606   $aAirplanes$xWings$2fast
606   $aLeading edges (Aerodynamics)$2fast
606   $aTrailing edge flaps$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xWings.
615  0$aLeading edges (Aerodynamics)
615  0$aTrailing edge flaps.
615  0$aWind tunnel testing.
615  7$aAirplanes$xWings.
615  7$aLeading edges (Aerodynamics)
615  7$aTrailing edge flaps.
615  7$aWind tunnel testing.
700   $aGauvain$b William E.$01408135
712 02$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   $a9910716799203321
996   $aWind-tunnel tests of a Clark Y wing with "Maxwell" leading-edge slots$93491293
997   $aUNINA