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010   $a9786610515646
010   $a1-84544-737-9
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100   $a20040205d2004      uy             0
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aNumerical methods in aerospace$b[electronic resource] $ecivil aviation and space exploration /$fM.A. Keavey
210   $aBradford, England $cEmerald Group$d2004
215   $a1 online resource (169 p.)
225 1 $aInternational Journal of Numerical methods for heat & fluid flow. No. 4 ;$vVol. 14
300   $aDescription based upon print version of record.
311   $a0-86176-958-9 
327   $aCONTENTS; 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 thrusters
330   $aTransonic flutter and active flap control, in two dimensions, are simulated by coupling independent structural dynamic and inviscid aerodynamic models, in the time domain. A flight control system, to actively control the trailing edge flap motion, has also been incorporated and, since this requires perfect synchronisation of fluid, structure and control signal, the ''strong'' coupling approach is adopted. The computational method developed is used to perform transonic aeroelastic and aeroservoelastic calculations in the time domain, and used to compute stability (flutter) boundaries of 2D wing
410  0$aInternational journal of numerical methods for heat & fluid flow ;$vv. 14, no. 4.
606   $aAeronautics
606   $aAstronautics
608   $aElectronic books.
615  0$aAeronautics.
615  0$aAstronautics.
676   $a629.1
676   $a629.108
700   $aKeavey$b M. A$0981177
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910449661203321
996   $aNumerical methods in aerospace$92239488
997   $aUNINA