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200 10$aAerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10? to 9.0 x 10? /$fby Laurence K. Loftin, Jr. and Hamilton A. Smith
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1949.
215   $a1 online resource (75 pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 1945
300   $a"October 1949."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 17).
517 3 $aAerodynamic characteristics of fifteen National Advisory Committee for Aeronautics airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)
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