LEADER 01657oam  2200493   450 
001 9910716990803321
005 20211026135611.0
035   $a(CKB)5470000002526284
035   $a(OCoLC)1154792929
035   $a(EXLCZ)995470000002526284
100   $a20200519d1939      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe unsteady lift of a finite wing /$fby Robert T. Jones
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1939.
215   $a1 online resource (13 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 682
300   $a"January 1939."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 13).
606   $aAirplanes$xWings
606   $aLift (Aerodynamics)
606   $aAspect ratio (Aerofoils)
606   $aAirplanes$xWings$2fast
606   $aLift (Aerodynamics)$2fast
615  0$aAirplanes$xWings.
615  0$aLift (Aerodynamics)
615  0$aAspect ratio (Aerofoils)
615  7$aAirplanes$xWings.
615  7$aLift (Aerodynamics)
700   $aJones$b Robert T$g(Robert Thomas),$f1910-1999,$01409563
712 02$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   $a9910716990803321
996   $aThe unsteady lift of a finite wing$93537122
997   $aUNINA