Author Index thin pane use control ind mathematical inverse *lastic syst iS USINZ Numerical Conunuation ee-ol-freedom twin-rotor multi-inpui multi-output system using radial iowaDdle eigenvector subspace nodelling techniques for simply-supporte, d surface tolerance on aircraft cost driver using numerical continuatior subspace Iitthh monmiontiotroirningg dati' a criitf ique . and laser Doppler anemometry experimental studies of a compressible short landing ground vort design of a solar-powered high-altitude very long endurance unmanned air vehicle ponse calculations e element contact method for use with Curvic couplings tems usl ng numerical continuation Euler scheme for pulse response calculations re-reinforced plastic hybrid composites under projectiles riutt cy" clel e oscilil ati, onns of { a contrtro l surface with free-play vr non' ocimetry and laser Doppler anemometry experimental . i compressible short ind vertical landing ground vortex flow ynamic surface tolerance or cost driver irious modelling techniques for simply-supported piezoelectric actuated thin panels elocimetry and laser Doppler anemometry experimental studies of a compressible short landing ground vortex flow of a curved beam under sinusoidal loading piecewise linear aeroelastic systems using numerical continuation 1erodynamic surface tolerance on aircraft cost driver ¥ mowuions of a body on a string ship's superstructure sinusoidal loading putation of aerodynamic parameters in hypersonic usoidal loading ince On aircraft cost driver flow and noise control contact meth or e with Curvic couplings near aecroeistl ystems using numerical continuation een wear processes and limit cycle oscillations of a control surface with free-play non motions of ; a string Non-linear modelling of < >-des reedom twin-rotor multi-input multi-output system using radial basis function networks AUTHOR INDEX ROCSAT