01252nam a22003375i 4500991002214019707536cr nn 008mamaa121227s1985 gw | s |||| 0|eng d9783540397434b14139054-39ule_instBibl. Dip.le Aggr. Matematica e Fisica - Sez. Matematicaeng512.5523512.48223AMS 30E10 AMS 41A10AMS 41A21AMS 42CPolynomes orthogonaux et applications[e-book] :proceedings of the laguerre symposium held at Bar-le-Duc, October 15-18, 1984 /edited by Claude Brezinski ... [et al.]Berlin :Springer,19851 online resource (xl, 588 p.)Lecture Notes in Mathematics,0075-8434 ;1171MathematicsTopological GroupsBrezinski, ClaudeSpringer eBookshttp://dx.doi.org/10.1007/BFb0076527An electronic book accessible through the World Wide Web.b1413905403-03-2205-09-13991002214019707536Polynomes orthogonaux et applications262633UNISALENTOle01305-09-13m@ -enggw 0001932oam 2200505Ia 450 991070190220332120260430112424.0(CKB)5470000002423101(OCoLC)804877134(DGPO)000876061(EXLCZ)99547000000242310120120806d1985 ua 0engtxtrdacontentcrdamediacrrdacarrierAnalysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed /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