01677oam 2200469 450 991071603070332120210525131139.0(CKB)5470000002517800(OCoLC)1150919711(EXLCZ)99547000000251780020200416d1936 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierWind-tunnel tests of wing flaps suitable for direct control of glide-path angle /by Fred E. WeickWashington, [D.C.] :National Advisory Committee for Aeronautics,1936.1 online resource (5 pages, 12 unnumbered pages) illustrationsTechnical note / National Advisory Committee for Aeronautics ;No. 552"January 1936."No Federal Depository Library Program (FDLP) item number.Includes bibliographical references (page 5).AirplanesWingsTestingAeronauticsResearchAeronauticsResearchfastAirplanesWingsTestingfastAirplanesWingsTesting.AeronauticsResearch.AeronauticsResearch.AirplanesWingsTesting.Weick Fred E.1387817United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910716030703321Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle3501185UNINA