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001 9910713882603321
005 20200825082824.0
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035   $a(OCoLC)1100474478
035   $a(EXLCZ)995470000002504865
100   $a20190508d1955      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aAerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds /$fby Bernard N. Daley and Douglas R. Lord
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1955.
215   $a1 online resource (57 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 3424
300   $a"May 1955."
300   $a"Supersedes recently declassified NACA RM L9E19. 1949"--Page 1.
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 10).
517 3 $aAerodynamic characteristics of several six-percent-thick airfoils at angles of attack from zero degrees to twenty degrees at high subsonic speeds
606   $aAerofoils$xTesting
606   $aAngle of attack (Aerodynamics)
606   $aAerofoils$xTesting$2fast
606   $aAngle of attack (Aerodynamics)$2fast
615  0$aAerofoils$xTesting.
615  0$aAngle of attack (Aerodynamics)
615  7$aAerofoils$xTesting.
615  7$aAngle of attack (Aerodynamics)
700   $aDaley$b Bernard N.$01404413
702   $aLord$b Douglas T.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
801  2$bOCLCO
801  2$bCOP
801  2$bTRAAL
801  2$bGPO
906   $aBOOK
912   $a9910713882603321
996   $aAerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds$93478941
997   $aUNINA