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. She is also core faculty in Global Studies and the Research Consortium on Gender-based Violence at MSU. She received her PhD in Philosophy and MA in Social and Political Theory from the University of ... & Political Philosophy, Feminisms of the Global South and Decolonial Theory. KRISTIE DOTSON is an Associate Professor of Philosophy at Michigan State University. She received her MA and PhD in Philosophy from
ideally just societies does not logically require the view that there is one best form of social organization,5 Sen argues that the emphasis on ideal theory in political philosophy bolsters the view that
An experimental investigation into the real-time flow and control characteristics of a flying wing with articulated winglets is described in this paper. The philosophy of the concept centres around
An experimental investigation into the real-time flow and control characteristics of a flying wing with articulated winglets is described in this paper. The philosophy of the concept centres around
An experimental investigation into the real-time flow and control characteristics of a flying wing with articulated winglets is described in this paper. The philosophy of the concept centres around
An experimental investigation into the real-time flow and control characteristics of a flying wing with articulated winglets is described in this paper. The philosophy of the concept centres around
to dynamic models consisting of a finite set of ordinary differential equations (ODEs). The helicopter model found using the philosophy summarized previously includes the fuselage, empennage, landing
to dynamic models consisting of a finite set of ordinary differential equations (ODEs). The helicopter model found using the philosophy summarized previously includes the fuselage, empennage, landing
to dynamic models consisting of a finite set of ordinary differential equations (ODEs). The helicopter model found using the philosophy summarized previously includes the fuselage, empennage, landing
and failure detection delay. The data-driven design philosophy was used in many parts of the overall FD procedure that is in the regressor selection phase for the considered sensors, in the design of
and failure detection delay. The data-driven design philosophy was used in many parts of the overall FD procedure that is in the regressor selection phase for the considered sensors, in the design of
and failure detection delay. The data-driven design philosophy was used in many parts of the overall FD procedure that is in the regressor selection phase for the considered sensors, in the design of
significantly the robustness in terms of false alarms and failure detection delay. The data-driven design philosophy was used in many parts of the overall FD procedure that is in the regressor selection phase for
all UPSat subsystems took place at AML/UPAT and LSF facilities following a non-COTS component philosophy, and the final assembly and integration were performed inside a clean room area (ISO-7) following
all UPSat subsystems took place at AML/UPAT and LSF facilities following a non-COTS component philosophy, and the final assembly and integration were performed inside a clean room area (ISO-7) following
all UPSat subsystems took place at AML/UPAT and LSF facilities following a non-COTS component philosophy, and the final assembly and integration were performed inside a clean room area (ISO-7) following
characteristics of flow and combustion because it allows for higher fidelity than RANS, at a lower computational cost than DNS [6–8]. The philosophy behind LES is to decompose turbulent motions into a grid-scale
areas [1]. Due to the increasing popularity of air travel and the rapid development of aeronautics in the past decades, aircraft noise has become not only an engineering problem but also a political and
lost due to the communication failure during the LEOP (Launch & Early Operational Phase). 2. Standard Platform Design 2.1. Main Philosophy for Standard Platform. The main objective of the standard
. Standard Platform Design2.1. Main Philosophy for Standard Platform The main objective of the standard platform developed in this study is to be able to include the requirements of various missions through
