Papers by Marilyn J Smith
EXTROVERT: Experience with Cross-Disciplinary Learning
Broadband Acoustic Flight Test Program for the Model 500E Helicopter
Continued Development of DME for Real-Time Spatial Positioning in Military Aircraft Testing
Improving UH-60 aeromechanics predictions with CFD and refined structural modeling
Issued as final report Center for Rotocraft Innovation
A Comparison of Turbulence Models for Aeroelastic Applications
Improvements to Helicopter 2-D Airfoil Design Using CFD Methodology
The transition from memorization of formulae to the independent thinking required in engineering ... more The transition from memorization of formulae to the independent thinking required in engineering courses is accomplished via courses typically entitled "Statics" and/or "Dynamics". These courses, in particular Dynamics pose a major hurdle for some students who wish to become engineers and are known at many universities as "hurdle" or "weed-out" courses. Since competency in the principles of these courses is necessary for success in the higher-level courses, teaching practices that improve a student's learning and motivation in the course are desired. This paper discusses a practice that has proven successful for a dynamics course that included students in different years and majors, as well as a class of sophomores of one major.
Rotorcraft Simulations Using Unstructured CFD-CSD Coupling
On the Conservation of CFD-CSD Coupling
Euler/Navier-Stokes Aeroelastic Analysis for Shell Structures
The Prediction and Validation of Static and Dynamic Stall
Georgia Tech Research Institute Georgia Institute of Technology Atlanta, Georgia
31 st Aerospace bciences Meeting & Exhibit
A fourth order Euler/Navier-Stokes prediction method for the aerodynamics and aeroelasticity of hovering rotor blades(Ph. D. Thesis)
Some of the computational issues relating to the development of a three-dimensional fourth-order ... more Some of the computational issues relating to the development of a three-dimensional fourth-order compact Euler/Navier-Stokes methodology for rotary wing flows and its coupling with an elastic rotor blade beam structural model have been explored. The compact Euler/NavierStokes method is used to predict the aerodynamic loads on an isolated rotor blade. Because the scheme is fourth-order, fewer grid nodes are necessary
Sources on an F-15-Like Wing ‘
A HYBRID FLOW ANALYSIS FOR ROTORS IN FORWARD FLIGHT
Advanced methods for predicting 3d unsteady flows around wind turbine blades
Innovative Strategies for Rotary-Wing Coupled Aeroelastic Simulations
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Papers by Marilyn J Smith