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100   $a20191113d1928      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of the Sperry Messenger fuselage on the air flow at the propeller plane /$fby Fred E. Weick
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1928.
215   $a1 online resource (5 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 274
300   $a"January 1928."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aWind tunnel testing
606   $aPropellers, Aerial
606   $aAir flow
606   $aWind tunnel testing$2fast
615  0$aWind tunnel testing.
615  0$aPropellers, Aerial.
615  0$aAir flow.
615  7$aWind tunnel testing.
700   $aWeick$b Fred E.$01387817
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713668203321
996   $aThe effect of the Sperry Messenger fuselage on the air flow at the propeller plane$93458781
997   $aUNINA