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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$aWind tunnel force tests in wing systems through large angles of attack /$fby Carl J. Wenzinger and Thomas A. Harris
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1928.
215   $a1 online resource (7 pages, 19 unnumbered pages) $cillustrations
225 1 $aTechnical notes / National Advisory Committee for Aeronautics ;$vNo. 294
300   $a"August 1928."
300   $aNo Federal Depository Library Program (FDLP) item number.
606   $aAirplanes$xWings$xTesting
606   $aWind tunnel testing
606   $aAngle of attack (Aerodynamics)
606   $aAirplanes$xWings$xTesting$2fast
606   $aAngle of attack (Aerodynamics)$2fast
606   $aWind tunnel testing$2fast
615  0$aAirplanes$xWings$xTesting.
615  0$aWind tunnel testing.
615  0$aAngle of attack (Aerodynamics)
615  7$aAirplanes$xWings$xTesting.
615  7$aAngle of attack (Aerodynamics)
615  7$aWind tunnel testing.
700   $aWenzinger$b Carl J$g(Carl Joseph),$f1903-1988,$01386955
702   $aHarris$b Thomas A.
712 02$aUnited States.$bNational Advisory Committee for Aeronautics,
801  0$bTRAAL
801  1$bTRAAL
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912   $a9910713659703321
996   $aWind tunnel force tests in wing systems through large angles of attack$93528964
997   $aUNINA