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100   $a20191113d1925      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe comparison of well-known and new wing sections tested in the variable density wind tunnel /$fby George J. Higgins
210  1$a[Washington, D.C.] :$cNational Advisory Committee for Aeronautics,$d1925.
215   $a1 online resource (13 pages, 30 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 219
300   $a"May 1925."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical reference (page 6).
606   $aAerofoils
606   $aWind tunnel testing
606   $aWind tunnel testing$2fast
606   $aAerofoils$xAerodynamics$2fast
615  0$aAerofoils.
615  0$aWind tunnel testing.
615  7$aWind tunnel testing.
615  7$aAerofoils$xAerodynamics.
700   $aHiggins$b George J.$01391744
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bTRAAL
801  2$bOCLCO
801  2$bOCLCF
801  2$bGPO
801  2$bSTF
801  2$bOCL
801  2$bGPO
906   $aBOOK
912   $a9910713555203321
996   $aThe comparison of well-known and new wing sections tested in the variable density wind tunnel$93545099
997   $aUNINA