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Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2001: Vol 215 Index PDF

3 Pages·2001·0.87 MB·English
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Preview Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 2001: Vol 215 Index

Author Index Active vibration control of a tr ng a lead zirconate titanate stack actuator Parametric modelling characterization of a two-degree-of-freedom twin-rotor multi-input multi-output Remote fan-lift engines Numerical predictions of turbule| nt und|e rexpanded sonic jets using a pressure-based methodology itivity study of the effects of manufacturing defects on the performance of a redundant hydraulic secondary flight control Comparison of numerical and ex nt nalyses for contact problems under normal and tangential 1] loads A low-mass multistage radiator for the passive cooling of X-ray charge-coupled devices in space A comparison of blade tip timing data analysis methods Testing of a novel ] propulsion system for micro air \ Parametric modell namic characterizationo f a two-degree-of-ff reedomn multi-input multi-o itput system Adaptive notch filter design for bending vibration of a sounding rocket ooper Flight test flutter prediction using neural networks ooper \ comparison of blade tip timing data analysis methods rowtner! Flight test fl utter predict 1 usIng neural networks Experimental aerodynan c characteristics of NAC A 0012 airfoils with simulated glaze and rime Debost. S \ panel with matche ylidene fluoride volume velocity sensor and uniform force actuator for the active control of sound transmission Dimitriadis, ¢ \ comparison of blade tip timing data analysis methods Ebrahimi, M Optima *| regulation Elferink, K OF; al and near-optimal take-off manoeuvres in the presence of windshear Elliott, S. J \ panel with matched polyvinylidene fluoride volume velocity sensor and uniform force actuator for the active control of sound transmission Experimental aerodynamic characteristics of NACA 0012 airfoils with simulated glaze and rime ice Phosphor thermometry in electron beam physical vapour deposition produced thermal barrier Foust, J P coating doped with dysprosium Frydrychewicz Aerodynamic, dynamic and conceptual design of a fire-fighting aircraft Fujimori, A A flight control design « vehicle using a double-loop control system with fuzzy gain- scheduling Gardonio, P \ panel with matched polyvinylidene fluoride volume velocity sensor and uniform force ictuator for the active control of sound transmission Gill, | An expert system for the determination of stress concentration factors Goodall, ¢ \ low-mass multistage radiator for the passive cooling of X-ray charge-coupled devices in space Gora}, Z Aerodynamic, dynamic an conceptual design of a fire-fighting aircraft Graham, R. H An expert system for the determination of stress concentration factors Gratton, G. B he weightshift-controlled microlight aeroplane Gupta M.M \ flight control design of a re-entry vehicle using a double-loop control system with fuzzy gain- scheduling leyes, A. | *hosphor thermometry in an electron beam physical vapour deposition produced thermal barrier coating doped with dysprosium \ combined testing and modelling approach to the prediction of the fretting fatigue performance of splined shafts Howe, D Blended wing body airframe mass prediction Hyde, T. H Finite element torsional buckling analysis of shafts with non-concentric bores Jin, H valuation of navigation errors based on ergodic processes Johnson, S. I Active vibration control of a space truss using a lead zirconate titanate stack actuator Kim, J Adaptive notch filter design for bending vibration of a sounding rocket ~ >3 Kuo, T.-¢ Blowdown and fluid hammer studies for a satellite reaction control subsystem 29] 700

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