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by
Phillips, Carrie A., author.
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theory is commonly used when describing ROS damage, but more insight is needed to be able to distinguish
by
Anishchenko, Ilya, author.
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modeling system dynamics and using airfoil theory, predicted dynamic response and simulated flight metrics
by
Chiu, Jack, author.
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system. Several solutions to this model which were solved using a Finite Difference approach are included
by
Gallaway, Scott, author.
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antenna array theory to determine the gain and beamwidth for antennas mounted to the wings. The results
by
Richter, Joseph P., author.
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overcome typical full appliance weighing difficulties. A system level model is developed which accounts for
by
Tangirala, Deepak Kumar, author.
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the theory of coordinate transformation and transformation matrix in the Diagnosis and Treatment Stage.
by
O'Dwyer, Martin Joseph, author.
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resolution of 0.96+-0.07ue was achieved over a range of 30,000ue. This system was used to characterise IFBG
by
Ghosh, K., author.
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, compressibility effect and hydrodynamic effect. The main objective was to produce an air bearing system capable of
by
Goudie, George O., author.
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earliest attempt to predict diffusion flame shape from diffusion theory is discussed. This theory is then
by
Bucsek, Ashley, author.
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microstructures are limited to those that are theoretically possible according to the Crystallographic Theory of
by
Erukulla, Gautami D., author.
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treated as an extensible elastic slender rod, and the Slender Rod Theory is thus used to derive the

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