00815nam0 2200265 450 00000770120081010082333.088-217-2312-720070313d2006----km-y0itay50------baitaITy-------001yy<<L' >>arbitratole novita della riformaD.Lgs. 2 febbraio 2006, n. 40Massimo CurtiMilanofioriAssagoIpsoa2006190 p.24 cmRiforma del processo civile62001Riforma del processo civileArbitrato<diritto privato>347.450920Curti,Massimo425339ITUNIPARTHENOPE20070313RICAUNIMARC000007701D-013839199NAVA32007Arbitrato721894UNIPARTHENOPE01931oam 2200553 450 991070619140332120170817140520.0(CKB)5470000002454509(OCoLC)858246894(EXLCZ)99547000000245450920130912j199812 ua 0engurbn||||a|a||txtrdacontentcrdamediacrrdacarrierEstimation of aircraft nonlinear unsteady parameters from wind tunnel data /Vladislav Klein, Patrick C. MurphyHampton, Virginia :National Aeronautics and Space Administration, Langley Research Center,December 1998.1 online resource (38 pages) illustrationsNASA TM ;1998-208969"December 1998.""Performing organization: NASA Langley Research Center"--Report documentation page.Includes bibliographical references (pages 16-17).Wind tunnel testsnasatUnsteady aerodynamicsnasatAerodynamic forcesnasatMathematical modelsnasatAircraft stabilitynasatFlight stability testsnasatWind tunnel tests.Unsteady aerodynamics.Aerodynamic forces.Mathematical models.Aircraft stability.Flight stability tests.Klein Vladislav1385898Murphy Patrick C.Langley Research Center,United States.National Aeronautics and Space Administration.OCLCEOCLCEOCLCOOCLCFOCLCQGPOBOOK9910706191403321Estimation of aircraft nonlinear unsteady parameters from wind tunnel data3434331UNINA