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035   $a(OCoLC)1136490269
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100   $a20200116d1929      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests /$fby Fred E. Weick and Donald H. Wood
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1929.
215   $a1 online resource (22 pages, 23 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 322
300   $a"October, 1929."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 6).
606   $aAirplanes$xWings
606   $aAirplanes$xMotors
606   $aDrag (Aerodynamics)
606   $aWind tunnel testing
606   $aAirplanes$xMotors$2fast
606   $aAirplanes$xWings$2fast
606   $aDrag (Aerodynamics)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xWings.
615  0$aAirplanes$xMotors.
615  0$aDrag (Aerodynamics)
615  0$aWind tunnel testing.
615  7$aAirplanes$xMotors.
615  7$aAirplanes$xWings.
615  7$aDrag (Aerodynamics)
615  7$aWind tunnel testing.
700   $aWeick$b Fred E.$01387817
702   $aWood$b Donald H.
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   $a9910713822003321
996   $aThe effect of the wings of single engine airplanes on propulsive efficiency as shown by full scale wind tunnel tests$93521469
997   $aUNINA