02988nam 2200601Ia 450 991044966120332120200520144314.01-280-51564-397866105156461-84544-737-9(CKB)1000000000005658(EBL)289851(OCoLC)70750563(SSID)ssj0000466077(PQKBManifestationID)11302554(PQKBTitleCode)TC0000466077(PQKBWorkID)10457862(PQKB)11774178(MiAaPQ)EBC289851(Au-PeEL)EBL289851(CaPaEBR)ebr10058610(CaONFJC)MIL51564(EXLCZ)99100000000000565820040205d2004 uy 0engur|n|---|||||txtccrNumerical methods in aerospace[electronic resource] civil aviation and space exploration /M.A. KeaveyBradford, England Emerald Group20041 online resource (169 p.)International Journal of Numerical methods for heat & fluid flow. No. 4 ;Vol. 14Description based upon print version of record.0-86176-958-9 CONTENTS; EDITORIAL ADVISORY BOARD; Abstracts and keywords; Editorial; Simulation of transonic flutter and active shockwave control; Numerical study of active shock control for transonic aerodynamics; Dynamic modeling in large-eddy simulation of turbulent channel flow Investigation of two-dimensional versus three-dimensional test filtering; The role of endothermic gasification in propellant ignition; Rarefied, superorbital flows in an expansion tube; Numerical simulation of inductively coupled plasma flows under chemical non-equilibrium; Discretization of the magnetic field in MPD thrustersTransonic flutter and active flap control, in two dimensions, are simulated by coupling independent structural dynamic and inviscid aerodynamic models, in the time domain. A flight control system, to actively control the trailing edge flap motion, has also been incorporated and, since this requires perfect synchronisation of fluid, structure and control signal, the ''strong'' coupling approach is adopted. The computational method developed is used to perform transonic aeroelastic and aeroservoelastic calculations in the time domain, and used to compute stability (flutter) boundaries of 2D wingInternational journal of numerical methods for heat & fluid flow ;v. 14, no. 4.AeronauticsAstronauticsElectronic books.Aeronautics.Astronautics.629.1629.108Keavey M. A981177MiAaPQMiAaPQMiAaPQBOOK9910449661203321Numerical methods in aerospace2239488UNINA