Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2006: Vol 220 Index PDF
Preview Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2006: Vol 220 Index
Author Index 2006 Allen, C B Development and validation of sliding and non-matching grid technology for control surface representation Ansari, SA Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 1: methodology and analysis Ansari, SA Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: implementation and validation Antoranz, J M a < B changes in Ti-6Al-2Sn-4Zr-2Mo-Si alloy: characterization, microstructure, and mechanical properties Avanzini, G Design of the flight management system for a shrouded-fan uninhabited aerial vehicle Badia, J M a «> B changes in Ti-6Al-2Sn-—4Zr-2Mo-Si alloy: characterization, microstructure, and mechanical properties Badcock, K Modelling three-dimensional dynamic stall of helicopter blades using computational fluid dynamics and neural networks Barakos, G Modelling three-dimensional dynamic stall of helicopter blades using computational fluid dynamics and neural networks Betz, D C Multi-functional fibre Bragg grating sensors for fatigue crack detection in metallic structures Bharani, S Effect of inlet swirl on the performance of annular diffusers having the same equivalent cone angle Biskri, D E Aerodynamic forces based on an error analytical formulation for aeroservoelasticity studies on an F/A-18 aircraft Bismarck-Nasr, M N Hybrid singular elements in fracture mechanics Boni, L Finite-element-based assessment of analytical methods for the design of fuselage frames Botez, R M Aerodynamic forces based on an error analytical formulation for aeroservoelasticity studies on an F/A-18 aircraft Catalano, F M Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets Ceron-Munoz, H D Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets Cheng, Y M Fault diagnosis of inertia sensor in missile control systems Chen, K-M Hybrid guidance law for interception of ballistic targets Chen, X M Suitability analysis of commercial off-the-shelf components for space application Chen, Y Square deployable frames for space applications. Part 1: theory Choi, J Measurements in the wake of an airfoil with regular roughness on the upper surface near the leading edge Chua, L P Kelvin-Helmholtz and streamwise vortices in the near wake of a single-lobe forced mixer Cui, MM Unsteady flow around suction elbow and inlet guide vanes in a centrifugal compressor Culshaw, B Multi-functional fibre Bragg grating sensors for fatigue crack detection in metallic structures Cummings, R M Continuing evolution of aerodynamic concept development using collaborative numerical and experimental evaluations de Matteis G Design of the flight management system for a shrouded-fan uninhabited aerial vehicle Evans, HE Oxidation of high-temperature coatings Fanteria, D Finite-element-based assessment of analytical methods for the design of fuselage frames Farrall, M Prediction of air/oil exit flows in a commercial aero-engine bearing chamber Fenwick, C L Development and validation of sliding and non-matching grid technology for control surface representation Fernandes, J L C Hybrid singular elements in fracture mechanics Finnis, M V Planar visualization of vortical flows Foord, CA High-speed ball bearing analysis Fujimori, A Model identification of linear parameter varying aircraft systerus Gao, H Investigation of cavitation near the orifice of hydraulic valves Gibson, A Modified stiffened panel analysis methods for laser beam and friction stir welded aircraft panels Giddings, D Prediction of air/oil exit flows in a commercial aero-engine bearing chamber Hay, J N Recent developments in thermoset curing methods He, X F Signal reconfiguration of missile fault-tolerant control © IMechE 2006 Proc. IMechE Vol. 220 Part G: J. Aerospace Engineering Author Index 2006 Heidebrecht, A \ numeric far field model for support interference studies in a slotted wall wind tunnel European Transonic Windtunnel Hess, RA Simplified approach for modelling pilot pursuit control behaviour in multi-loop flight control tasks Hibberd, S Prediction of air/oil exit flows in a commercial aero-engine bearing chamber Houdeville, R lransition measurement and prediction on a generic high-lift swept wing Huang, S-W Hybrid guidance law for interception of ballistic targets Hu, Q Optimal sliding mode manoeuvring control and active vibration reduction of flexible spacecraft Hummel, D Che Second International Vortex Flow Experiment (VFE-2): Objectives and First Results Jiang, X J Suitability analysis of commercial off-the-shelf components for space application Khan, M K Compressive and lamination strength of honeycomb sandwich panels with strain energy calculation from: ASTM standards Kim, H-D Influence of the nozzle inlet configuration on under-expanded swirling jet Kim, |]S Measurements in the wake of an airfoil with regular roughness on the upper surface near the leading edge Kim, M Coulomb formation conservation laws using differential orbit elements Kim, S Measurements in the wake of an airfoil with regular roughness on the upper surface near the leading edge Knowle Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 1: methodology and analysis Knowle \ review of jet mixing enhancement for aircraft propulsion applications Knowle Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: implementation and validation Knowle Planar visualization of vortical flows Knowle Planar visualization of vortical flows Kolar, \ Vorticity and circulation aspects of twin jets in cross-flow for an oblique nozzle arrangement Lee, K-H Influence of the nozzle inlet configuration on under-expanded swirling jet Liang, Y Fault diagnosis of inertia sensor in missile control systems Lin, C-l Hybrid guidance law for interception of ballistic targets Lin, W Investigation of cavitation near the orifice of hydraulic valves Liu, X ¢ Fault diagnosis of inertia sensor in missile control systems Liu X ( Signal reconfiguration of missile fault-tolerant control Lyung,| Model identification of linear parameter varying aircraft systems Lynch, I Modified stiffened panel anaiysis methods for laser beam and friction stir welded aircraft panels Ma, G Optimal sliding mode manoeuvring control and active vibration reduction of flexible spacecralt Mao, RH Kelvin—Helmholtz and streamwise vortices in the near wake of a single-lobe forced mixer Matsuo, S Influence of the nozzle inlet configuration on under-expanded swirling jet McGuirk, J J Prediction of a non-isothermal three-dimensional mixing layer created by a scarfed lobed mixer Mehrabian, A R Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique Mills, A Development of an automated preforming technology for resin infusion processing of air- crait components Moens, | rransition measurement and prediction on a generic high-lift swept wing Morinigo, J A lhree-dimensional simulation of the self-oscillating flow and side-loads in an over- expanded subscale rocket nozzle Morton, SA Continuing evolution of aerodynamic concept development using collaborative numerical and experimental evaluations Murphy, A Modified stiffened panel analysis methods for laser beam and friction stir welded aircraft panels Newman, S } \ full-span free-wake model using circular-arc vortex elements and incorporating rotor trim analysis © Gara P Recent developments in thermoset curing methods Okamoto, S Vorticity and circulation aspects of twin jets in cross-flow for an oblique nozzle arrangement Page, G J Prediction of a non-isothermal three-dimensional mixing layer created by a scarfed lobed mixer Pan, Q Fault diagnosis of inertia sensor in missile control systems Park, J Measurements in the wake of an airfoil with regular roughness on the upper surface near the leading edge Perraud, J rransition measurement and prediction on a generic high-lift swept wing Piris, NM a < B changes in Ti-6Al-2Sn-—4Zr-—2Mo-Si alloy: characterization, microstructure, and mechanical properties Price, M Modified stiffened panel analysis methods for laser beam and friction stir welded aircraft panels Richards, B Modelling three-dimensional dynamic stall of helicopter blades using computational fluid dynamics and neural networks Proc. IMechE Vol. 220 Part G: J.A erospace Engineering Author Index 2006 Rodriguez, M C a <> B changes in Ti-6Al—2Sn—4Zr-—2Mo-Si alloy: characterization, microstructure, and mechanical properties Roshanian, J Skid-to-turn missile autopilot design using scheduled eigenstructure assignment technique Saddington, A J A review of jet mixing enhancement for aircraft propulsion applications Saddington, A J Planar visualization of vortical flows Saha, K Effect of inlet swirl on the performance of annular diffusers having the same equivalent cone angle Salman, H Prediction of a non-isothermal three-dimensional mixing layer created by a scarfed lobed mixer Salva, J J Three-dimensional simulation of the self-oscillating flow and side-loads in an over- expanded subscale rocket nozzle Sarigul-Klijn, M A comparative analysis of methods for air-launching vehicles from earth to sub-orbit or orbit Sarigul-Klijn, N A comparative analysis of methods for air-launching vehicles from earth to sub-orbit or orbit Savory, E Vorticity and circulation aspects of twin jets in cross-flow for an oblique nozzle arrangement Schaub, H Coulomb formation conservation laws using differential orbit elements Seshadri, V Effect of inlet swirl on the performance of annular diffusers having the same equivalent cone angle Setoguchi, T Influence of the nozzle inlet configuration on under-expanded swirling jet Simmons, K Prediction of air/oil exit flows in a commercial aero-engine bearing chamber Simon, AG a < B changes in Ti-6Al-2Sn-—4Zr-—2Mo-Si alloy: characterization, microstructure, and mechanical properties Singh, S N Effect of inlet swirl on the performance of annular diffusers having the same equivalent cone angle Spentzos, A Modelling three-dimensional dynamic stall of helicopter blades using computational fluid dynamics and neural networks Séraudie, A rransition measurement and prediction on a generic high-lift swept wing Staszewski, W J Multi-functional fibre Bragg grating sensors for fatigue crack detection in metallic structures Sundaresan, M Design aspects of launch vehicle sizing including air-breathing propulsion Sun, H X Suitability analysis of commercial off-the-shelf components for space application Takao, H Vorticity and circulation aspects of twin jets in cross-flow for an oblique nozzle arrangement arin, P a < B changes in Ti-6Al-2Sn—4Zr-—2Mo-Si alloy: characterization, microstructure, and mechanical properties Taylor, M P Oxidation of high-temperature coatings Thursby, G Multi-functional fibre Bragg grating sensors for fatigue crack detection in metallic structures lodoroki, T Vorticity and circulation aspects of twin jets in cross-flow for an oblique nozzle arrangement Toy, N Vorticity and circulation aspects of twin jets in cross-flow for an oblique nozzle arrangement sukiji, 1 Investigation of cavitation near the orifice of hydraulic valves van Muijden J Improvement and verification of low-speed aerodynamic characteristics of a supersonic civil transport aircraft Vempati, K K Effect of inlet swirl on the performance of annular diffusers having the same equivalent cone angle Wang, Z H Suitability analysis of commercial off-the-shelf components for space application Wen, B C Neural network for structural stress concentration factors in reliability-based optimization Wu, M-T Hybrid guidance law for interception of ballistic targets Xiao, L X Signal reconfiguration of missile fault-tolerant control Xu, GH A full-span free-wake model using circular-arc vortex elements and incorporating rotor trim analysis Xu, J H Signal reconfiguration of missile fault-tolerant control Yang, A-S Plume impingement investigation using Monte-Carlo computations You, Z Square deployable frames for space applications. Part 1: theory Yuan, Q Fault diagnosis of inertia sensor in missile control systems Yu, GH Suitability analysis of commercial off-the-shelf components for space application Yu,SCM Kelvin-Helmholtz and streamwise vortices in the near wake of a single-lobe forced mixer Zbikowski, R Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 1: methodology and analysis Zbikowski, R Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: implementation and validation Zhang, H C Fault diagnosis of inertia sensor in missile control systems Zhang,L Neural network for structural stress concentration factors in reliability-based optimization Zhang, L Suitability analysis of commercial off-the-shelf components for space application Zhang, Y M Neural network for structural stress concentration factors in reliability-based optimization Zhao, T L Suitability analysis of commercial off-the-shelf components for space application Zheng, J X Neural network for structural stress concentration factors in reliability-based optimization Zhou, C Y Suitability analysis of commercial off-the-shelf components for space application WW&XY UeOOhrIe NSKK S NNNNN © IMechE 2006 Proc. IMechE Vol. 220 Part G: J. Aerospace Engineering
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