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100   $a20190508d1951      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow /$fby Chieh-Chien Chang
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1951.
215   $a1 online resource (76 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 2467
300   $a"October 1951."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 57).
606   $aAirplanes$xWings, Swept-back
606   $aOscillating wings (Aerodynamics)
606   $aAerodynamics, Supersonic
606   $aAerodynamics, Supersonic$2fast
606   $aAirplanes$xWings, Swept-back$2fast
606   $aOscillating wings (Aerodynamics)$2fast
615  0$aAirplanes$xWings, Swept-back.
615  0$aOscillating wings (Aerodynamics)
615  0$aAerodynamics, Supersonic.
615  7$aAerodynamics, Supersonic.
615  7$aAirplanes$xWings, Swept-back.
615  7$aOscillating wings (Aerodynamics)
700   $aZhang$b Jieqian$01401173
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bCOP
801  2$bTRAAL
801  2$bGPO
906   $aBOOK
912   $a9910713754503321
996   $aThe aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow$93469530
997   $aUNINA