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100   $a20190610d1951      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAir forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow /$fby Charles E. Watkins
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1951.
215   $a1 online resource (44 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2457
300   $a"September 1951."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 34).
606   $aAirplanes$xWings, Swept-back
606   $aAirplanes$xWings, Triangular
606   $aLeading edges (Aerodynamics)
606   $aOscillating wings (Aerodynamics)
606   $aAirplanes$xWings, Swept-back$2fast
606   $aAirplanes$xWings, Triangular$2fast
606   $aLeading edges (Aerodynamics)$2fast
606   $aOscillating wings (Aerodynamics)$2fast
615  0$aAirplanes$xWings, Swept-back.
615  0$aAirplanes$xWings, Triangular.
615  0$aLeading edges (Aerodynamics)
615  0$aOscillating wings (Aerodynamics)
615  7$aAirplanes$xWings, Swept-back.
615  7$aAirplanes$xWings, Triangular.
615  7$aLeading edges (Aerodynamics)
615  7$aOscillating wings (Aerodynamics)
700   $aWatkins$b Charles E.$0303474
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bTRAAL
801  2$bOCLCF
801  2$bGPO
906   $aBOOK
912   $a9910713754703321
996   $aAir forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow$93462045
997   $aUNINA