LEADER 01771oam  2200517   450 
001 9910716737003321
005 20210824141202.0
035   $a(CKB)5470000002524807
035   $a(OCoLC)1159597610
035   $a(EXLCZ)995470000002524807
100   $a20200623d1937      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aEmpirical corrections to the span load distribution at the tip /$fby H.A. Pearson
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1937.
215   $a1 online resource (10 pages, 6 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 606
300   $a"August 1937."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (pages 9-10).
606   $aAirplanes$xWings
606   $aAerodynamic load
606   $aMathematical models
606   $aAerodynamic load$2fast
606   $aAirplanes$xWings$2fast
606   $aMathematical analysis$2fast
615  0$aAirplanes$xWings.
615  0$aAerodynamic load.
615  0$aMathematical models.
615  7$aAerodynamic load.
615  7$aAirplanes$xWings.
615  7$aMathematical analysis.
700   $aPearson$b Henry A$g(Henry Adolph),$f1906-$01398867
712 02$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   $a9910716737003321
996   $aEmpirical corrections to the span load distribution at the tip$93483587
997   $aUNINA