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001 9910713081003321
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100   $a20190703d1922      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEffect of aerofoil aspect ratio on the slope of the lift curve /$fby Walter S. Diehl
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1922.
215   $a1 online resource (4 pages, 1 unnumbered page) $cillustration
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 79
300   $a"January, 1922."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aAerofoils
606   $aAerofoils$xMathematical models
606   $aAspect ratio (Aerofoils)
606   $aLift (Aerodynamics)
606   $aAerofoils$2fast
606   $aAerofoils$xMathematical models$2fast
606   $aAspect ratio (Aerofoils)$2fast
606   $aLift (Aerodynamics)$2fast
615  0$aAerofoils.
615  0$aAerofoils$xMathematical models.
615  0$aAspect ratio (Aerofoils)
615  0$aLift (Aerodynamics)
615  7$aAerofoils.
615  7$aAerofoils$xMathematical models.
615  7$aAspect ratio (Aerofoils)
615  7$aLift (Aerodynamics)
700   $aDiehl$b Walter S$g(Walter Stuart),$f1893-1976,$0304962
712 02$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   $a9910713081003321
996   $aEffect of aerofoil aspect ratio on the slope of the lift curve$93529551
997   $aUNINA