Browsing by Author "Strganac, Thomas W"
Now showing items 1-12 of 12
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Babbar, Yogesh (2015-05-12)Aeroservoelasticity (ASE) is the interdisciplinary study of the interaction of structural, inertial, aerodynamic, and control loads for aircraft systems, and is inherently a nonlinear phenomenon. One of the goals of ASE ...
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Beckett, Andrew 1984- (2012-11-12)Intelligence, surveillance, and reconnaissance unmanned aircraft systems (UAS) are the most common variety of UAS in use today and provide invaluable capabilities to both the military and civil services. Keeping the sensors ...
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Strganac, Thomas W (Texas A&M University, 1980)Not available
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Henrickson, James V (2014-04-28)Shape memory alloys are capable of delivering advantageous solutions to a wide range of engineering-based problems. Implementation of these solutions, however, is often complicated by the hysteretic, non-linear, thermomechanical ...
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Ehrmann, Robert Schaefer (2014-06-25)Wind farm operators observe production deficits as machines age. Quantifying deterioration on individual components is difficult, but one potential explanation is accumulation of blade surface roughness. Historically, wind ...
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Leaton, Andrew (2020-06-11)Aircraft noise is a source of disruption and annoyance to those living within close proximity to airports. Airframe noise is a main contributor to the overall noise level created by aircraft during approach and landing. ...
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May, James F (2013-03-18)A need has arisen for an easy-to-use, flexible, transparent, and cross-platform communication backbone for configuration and execution of distributed simulations and experiments. Open source, open architecture, and custom ...
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Suryakumar, Vishvas Samuel (2013-05-02)A co-simulation methodology is explored whereby a finite element code and a multi-body dynamics code featuring flexible cantilevered beams can be coupled and interactively executed. The floating frame of reference formulation ...
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Suryakumar, Vishvas Samuel (2016-12-12)Recent experiments have suggested a strong correlation between local flow features on the airfoil surface such as the leading edge stagnation point (LESP), transition or the flow separation point with global integrated ...
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Rollins, Elizabeth (2013-09-03)Because of the widely varying flight conditions in which hypersonic vehicles operate and certain aspects unique to hypersonic flight, the development of control architectures for these vehicles presents a challenge. Previous ...
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Owens, Brian C (2013-11-07)The availability of offshore wind resources in coastal regions along with a high concentration of load centers in these areas makes offshore wind energy an attractive opportunity. Infrastructure costs and operation and ...
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Liliedahl, David Noel (2017-06-21)A time-linearized CFD solver for analyzing rotordynamics of gas seals is presented offering an improvement over existing linearized CFD solvers. Previous linearized solvers required structured grids and axisymmetric domains, ...