01927oam 2200493Ia 450 991070190220332120120806144759.0(CKB)5470000002423101(OCoLC)804877134(EXLCZ)99547000000242310120120806d1985 ua 0engtxtrdacontentcrdamediacrrdacarrierAnalysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed[electronic resource] /by Arthur F. SmithWindsor Locks, Conn. :Hamilton Standard Division, United Technologies Corporation ;Cleveland, Ohio :National Aeronautics and Space Administration, Lewis Research Center,[1985]1 online resource (x, 101/102 pages) illustrationsNASA CR ;175026Title from title screen (viewed on Aug. 6, 2012)."December, 1985."Includes bibliographical references (page 29/30).Aerodynamic stabilitynasatDynamic responsenasatDynamic structural analysisnasatEvaluationnasatProp-fan technologynasatTurboprop enginesnasatAerodynamic stability.Dynamic response.Dynamic structural analysis.Evaluation.Prop-fan technology.Turboprop engines.Smith Arthur F130914Lewis Research Center.United Technologies Corporation.Hamilton Standard Division.GPOGPOGPOBOOK9910701902203321Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed3495404UNINA