<h1>Rowley, Clarence Worth</h1> <h2>Conference Item from <a href="https://authors.library.caltech.edu">CaltechAUTHORS</a></h2> <ul> <li>Colonius, T. and Rowley, C. W., el al. (2019) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190726-104730024">Global Instabilities and Reduced-Order Models of Cavity Flow Oscillations</a></li> <li>Taira, Kunihiko and Rowley, Clarence W., el al. (2010) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190717-102320131">Feedback Control of High-Lift State for A Low-Aspect-Ratio Wing</a>; <a href="https://doi.org/10.2514/6.2010-357">10.2514/6.2010-357</a></li> <li>Williams, David and Quach, Vien, el al. (2009) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190717-102319638">Low Reynolds Number Wing Response to an Oscillating Freestream With and Without Feed Forward Control</a>; <a href="https://doi.org/10.2514/6.2009-143">10.2514/6.2009-143</a></li> <li>Tadmor, Gilead and Williams, David R., el al. (2008) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190717-102320405">Control of a Semi-Circular Planform Wing in a "Gusting" Unsteady Free Stream Flow II: Modeling and Feedback Design</a>; <a href="https://doi.org/10.2514/6.2008-3977">10.2514/6.2008-3977</a></li> <li>Rowley, Clarence W. and Ahuja, Sunil, el al. (2008) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190717-102320932">Closed-Loop Control of Leading Edge Vorticity on a 3D Wing: Simulations and Low-Dimensional Models</a>; <a href="https://doi.org/10.2514/6.2008-3981">10.2514/6.2008-3981</a></li> <li>Brunton, Steven L. and Rowley, Clarence W., el al. (2008) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190718-165125978">Unsteady Aerodynamic Forces on Small-Scale Wings: Experiments, Simulations, and Models</a>; <a href="https://doi.org/10.2514/6.2008-520">10.2514/6.2008-520</a></li> <li>Ahuja, Sunil and Rowley, Clarence W., el al. (2007) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190718-165125547">Low-Dimensional Models for Control of Leading-Edge Vortices: Equilibria and Linearized Models</a>; <a href="https://doi.org/10.2514/6.2007-709">10.2514/6.2007-709</a></li> <li>Taira, Kunihiko and Dickson, William B., el al. (2007) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190718-165127033">Unsteadiness in Flow over a Flat Plate at Angle-of-Attack at Low Reynolds Numbers</a>; <a href="https://doi.org/10.2514/6.2007-710">10.2514/6.2007-710</a></li> <li>Rowley, Clarence W. and Williams, David R., el al. (2002) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190709-092100972">Model-based control of cavity oscillations. II - System identification and analysis</a>; <a href="https://doi.org/10.2514/6.2002-972">10.2514/6.2002-972</a></li> <li>Williams, David R. and Rowley, Clarence W., el al. (2002) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190718-165126408">Model-based control of cavity oscillations. I - Experiments</a>; <a href="https://doi.org/10.2514/6.2002-971">10.2514/6.2002-971</a></li> <li>Rowley, Clarence W. and Colonius, Tim, el al. (2001) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190726-104731145">Dynamical models for control of cavity oscillations</a>; <a href="https://doi.org/10.2514/6.2001-2126">10.2514/6.2001-2126</a></li> <li>Rowley, Clarence W. and Colonius, Tim, el al. (2000) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190726-104731320">POD Based Models of Self-Sustained Oscillations in the Flow Past an Open Cavity</a>; <a href="https://doi.org/10.2514/6.2000-1969">10.2514/6.2000-1969</a></li> <li>Colonius, Tim and Basu, Amit J., el al. (1999) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190726-104730595">Numerical investigation of the flow past a cavity</a>; <a href="https://doi.org/10.2514/6.1999-1912">10.2514/6.1999-1912</a></li> <li>Rowley, Clarence W. and Colonius, Tim (1998) <a href="https://resolver.caltech.edu/CaltechAUTHORS:20190726-104731244">Numerically nonreflecting boundary conditions for multidimensional aeroacoustic computations</a>; <a href="https://doi.org/10.2514/6.1998-2220">10.2514/6.1998-2220</a></li> </ul>