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100   $a20200206d1931      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe pressure distribution over a modified elliptical wing tip on a biplane in flight /$fby Richard V. Rhode and Eugene E. Lundquist
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1931.
215   $a1 online resource (14 pages, 8 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 387
300   $a"August, 1931."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 4).
606   $aBiplanes
606   $aAirplanes$xWings
606   $aAerodynamic load$xTesting
606   $aAerodynamic load$xTesting$2fast
615  0$aBiplanes.
615  0$aAirplanes$xWings.
615  0$aAerodynamic load$xTesting.
615  7$aAerodynamic load$xTesting.
700   $aRhode$b Richard V.$01386735
702   $aLundquist$b Eugene E.
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   $a9910715130403321
996   $aThe pressure distribution over a modified elliptical wing tip on a biplane in flight$93492174
997   $aUNINA