00957nam0-22003251i-450-99000045407040332120070626104625.0000045407FED01000045407(Aleph)000045407FED0100004540720020821d1961----km-y0itay50------baenga-------001yyAdaptive control systemsEli Mishkin, Ludwig BraunNew York [etc.]McGraw-Hill1961533 p.ill.23 cmMcGraw-Hill electrical and electronic engineering seriesBrooklyn Polytechnic Institute seriesSistemi retroazionati629.83Mishkin,Eli25254Braun,Ludwig25255ITUNINARICAUNIMARCBK99000045407040332110 D III 233900DINELDINELAdaptive control systems334211UNINA02113oam 2200589 450 991071344760332120200428091842.0(CKB)5470000002501178(OCoLC)1117765907(EXLCZ)99547000000250117820190909d1923 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierCalculations for a single-strut biplane with reference to the tensions in the wing bracing /by O. Blumenthal[Washington, D.C.] :National Advisory Committee for Aeronautics,1923.1 online resource (28 pages, 3 unnumbered pages) illustrationsTechnical notes / National Advisory Committee for Aeronautics ;No. 143"June 1923.""From Technische Berichte, Vol. III, No. 5.""Translated by National Advisory Committee for Aeronautics"--Page 28.No Federal Depository Library Program (FDLP) item number.Includes bibliographical references.AirplanesWingsStrains and stressesStruts (Engineering)Mathematical modelsAirplanesWingsfastMathematical modelsfastStrains and stressesfastStruts (Engineering)fastAirplanesWings.Strains and stresses.Struts (Engineering)Mathematical models.AirplanesWings.Mathematical models.Strains and stresses.Struts (Engineering)Blumenthal Otto1876-1944,54552United States.National Advisory Committee for Aeronautics,TRAALTRAALOCLCOOCLCFGPOBOOK9910713447603321Calculations for a single-strut biplane with reference to the tensions in the wing bracing3528994UNINA