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100   $a20200416d1936      ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aWind-tunnel tests of wing flaps suitable for direct control of glide-path angle /$fby Fred E. Weick
210  1$aWashington, [D.C.] :$cNational Advisory Committee for Aeronautics,$d1936.
215   $a1 online resource (5 pages, 12 unnumbered pages) $cillustrations
225 1 $aTechnical note / National Advisory Committee for Aeronautics ;$vNo. 552
300   $a"January 1936."
300   $aNo Federal Depository Library Program (FDLP) item number.
320   $aIncludes bibliographical references (page 5).
606   $aAirplanes$xWings$xTesting
606   $aAeronautics$xResearch
606   $aAeronautics$xResearch$2fast
606   $aAirplanes$xWings$xTesting$2fast
615  0$aAirplanes$xWings$xTesting.
615  0$aAeronautics$xResearch.
615  7$aAeronautics$xResearch.
615  7$aAirplanes$xWings$xTesting.
700   $aWeick$b Fred E.$01387817
712 02$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   $a9910716030703321
996   $aWind-tunnel tests of wing flaps suitable for direct control of glide-path angle$93501185
997   $aUNINA