LEADER 01644oam  2200469   450 
001 9910715346103321
005 20210226094833.0
035   $a(CKB)5470000002510574
035   $a(OCoLC)1145759599
035   $a(EXLCZ)995470000002510574
100   $a20200323d1934      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aTests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections /$fby Raymond F. Anderson
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1934.
215   $a1 online resource (8 pages, 5 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 487
300   $a"January 1934."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aAerofoils
606   $aWind tunnel testing
606   $aAerodynamics
606   $aAerodynamics$2fast
615  0$aAerofoils.
615  0$aWind tunnel testing.
615  0$aAerodynamics.
615  7$aAerodynamics.
700   $aAnderson$b Raymond F.$091081
712 02$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   $a9910715346103321
996   $aTests of three tapered airfoils based on the N.A.C.A. 2200, the N.A.C.A.-M6, and the Clark Y sections$93522095
997   $aUNINA