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035   $a(EXLCZ)995470000002504804
100   $a20190610d1954      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamics of slender wings and wing-body combinations having swept trailing edges /$fby Harold Mirels
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1954.
215   $a1 online resource (ii, 96 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3105
300   $a"March 1954."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 73-75).
606   $aAerodynamics
606   $aAir flow
606   $aAirplanes$xWings, Swept-back
606   $aIntegral equations
606   $aTrailing edges (Aerodynamics)
606   $aAerodynamics$2fast
606   $aAir flow$2fast
606   $aAirplanes$xWings, Swept-back$2fast
606   $aIntegral equations$2fast
606   $aTrailing edges (Aerodynamics)$2fast
615  0$aAerodynamics.
615  0$aAir flow.
615  0$aAirplanes$xWings, Swept-back.
615  0$aIntegral equations.
615  0$aTrailing edges (Aerodynamics)
615  7$aAerodynamics.
615  7$aAir flow.
615  7$aAirplanes$xWings, Swept-back.
615  7$aIntegral equations.
615  7$aTrailing edges (Aerodynamics)
700   $aMirels$b Harold$01416564
712 02$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   $a9910713888603321
996   $aAerodynamics of slender wings and wing-body combinations having swept trailing edges$93527533
997   $aUNINA