Spelling suggestions: "subject:"airplanes"" "subject:"airplane’s""
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Aircraft : nationality and cooperative arrangementsSirag-Eldin, Yahya January 1977 (has links)
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The effects of radius of arc of turn size, speed turn rate, and angle of turn upon the accuracy of a turn onto a runway in a simulated air traffic control task /Wachsler, Robert Allen January 1958 (has links)
No description available.
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Photochemical initiation of combustion and quantum yields in flowing mixtures of hydrogen, oxygen and chlorine /Lawrence, Lloyd Robert January 1969 (has links)
No description available.
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The effect of pilot restraint and aerodynamic forces on the flutter of reversible control systems /Murphy, John Allen January 1970 (has links)
No description available.
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Theory of an air cushion landing system for aircraft /Digges, Kennerly Hite January 1971 (has links)
No description available.
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Attrition of bombers as a function of weapon load and grouping of the airborne defense /Jones, Chester George January 1971 (has links)
No description available.
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An investigation of a sequential multiple look pattern recognition system for automatic aircraft identification /Yeh, James Yung-Shao January 1976 (has links)
No description available.
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Aircraft agilityThompson, Brian G. 19 September 2009 (has links)
A definition of an aircraft agility vector is given as the time rate-of-change of the applied forces acting on an aircraft and agility is characterized as being representable by instantaneous and integral time-scales. A unified framework for evaluating instantaneous and integral agility is developed based on the notion of a new dynamic model for aircraft motions. This model may be viewed as intermediate between a point-mass model, in which the body attitude angles are control-like, and a rigid-body model, in which the body attitude angles evolve according to Newton's Laws. Specifically, we consider the case of symmetric flight and construct a model in which the body roll-rate and pitch-rate are the controls. Accordingly, we refer to this new dynamics model as the body-rate model, (BRM).
Instantaneous agility is presented as the locus of achievable agility vectors and the construction of such agility sets is demonstrated from aerodynamic and propulsive data for a modern jet fighter. Figures depicting this locus are displayed with indications of the limiting control. An integral performance flight problem is presented and subsequently solved via the optimal control theory. Agility metrics are suggested for this problem based on the transients which exist between the dynamics of the BRM and those of the point-mass model. Suggestions are also provided on the use of instantaneous agility sets and integral agility metrics in the design of aircraft and in performance comparisons of competing aircraft. / Master of Science
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In-situ structural health monitoring of composite repair patchesKoh, Yeow Leung, 1976- January 2002 (has links)
Abstract not available
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Flow management in heat exchanger installations for intercooled turbofan enginesKwan, Pok Wang January 2011 (has links)
No description available.
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