01070nam--2200349---450-99000606424020331620150806121856.0000606424USA01000606424(ALEPH)000606424USA0100060642420150804d1898----km-y0itay50------baitaIT||||||||001yy<<La>> fanciulletta italiana educata e istruitaletture per la seconda classe elementare femminileBartolomeo RinaldiNovissima edTorinoLibreria Scolastica di Grato Scioldo1898191 p.ill.19 cm20012001808.899 282BNCFRINALDI,Bartolomeo196003ITsalbcISBD990006064240203316XV.7. 118130 FCarXV.7.378520BKFCARGENEROSO9020150804USA011041ALESSANDRA9020150806USA011218Fanciulletta italiana educata e istruita1102125UNISA01751nam 2200481I 450 991070574900332120170623064941.0(CKB)5470000002452917(OCoLC)990800988(EXLCZ)99547000000245291720170623d1995 ua 0engurbn|||||||||txtrdacontentcrdamediacrrdacarrierOptimization of an advanced design three-element airfoil at high Reynolds numbers /J.C. Lin, C.J. Dominik[Washington, D.C.]:National Aeronautics and Space Administration,[1995].1 online resource (11 pages) illustrationsNASA-TM ;112019"AIAA 13th Applied Aerodynamics Conference, June 19-22, 1995, San Diego, CA.""AIAA 95-1858."Includes bibliographical references (page 11).AirfoilsnasatComputational fluid dynamicsnasatHigh Reynolds numbernasatLeading edgesnasatPrediction analysis techniquesnasatAirfoils.Computational fluid dynamics.High Reynolds number.Leading edges.Prediction analysis techniques.Lin J.-C(Jiun-Chuan),612234Dominik C. J.American Institute of Aeronautics and Astronautics.United States.National Aeronautics and Space Administration,GPOGPOBOOK9910705749003321Optimization of an advanced design three-element airfoil at high Reynolds numbers3468132UNINA