Flexible Launch Vehicle Stability Analysis Using Steady and Unsteady Computational Fluid Dynamics von Bartels, Robert E

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Flexible Launch Stability Analysis Using Steady and Unsteady Computational Fluid Dynamics von Bartels, Robert E

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Aeroservoelastic Test of the Subsonic Ultra-Green Aircraft Research Truss-Braced Wing Model von Scott, Robert C., Bartels, Robert E., Funk, Christie J., Allen, Timothy J, Sexton, Bradley W., Dykman, John R., Coulson, David A.

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Computational Aeroelastic Analysis of the Ares I Crew Launch Vehicle During Ascent von Bartels, Robert E, Chwalowski, Pawel, Massey, Steven J, Heeg, Jennifer, Mineck, Raymond E

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Computations of Wall Distances Based on Differential Equations von Tucker, Paul G, Rumsey, Chris L, Spalart, Philippe R, Bartels, Robert E, Biedron, Robert T

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Improved Flutter Boundary Prediction for an Isolated Two-Degree-of-Freedom Airfoil von Schwarz, Jordan B, Dowell, Earl H, Thomas, Jeffrey P, Hall, Kenneth C, Rausch, Russ D, Bartels, Robert E

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Mesh Strategies for Accurate Computation of Unsteady Spoiler and Aeroelastic Problems von Bartels, Robert E

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Comparison of Two Navier-Stokes Methods with Benchmark Active Control Technology Experiments von Bartels, Robert E, Schuster, David M

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Computational Fluid Dynamics Simulations of the Transonic Dynamics Tunnel Airstream Oscillator System von Bartels, Robert E, Chwalowski, Pawel

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A time integration algorithm based on the state transition matrix for structures with time varying and nonlinear properties von Bartels, Robert E.

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Flexible Launch Stability Analysis Using Steady and Unsteady Computational Fluid Dynamics von Bartels, Robert E

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Computation of Wall Distance Based on Differential Equations von Tucker, Paul G, Rumsey, Chris L, Spalart, Philippe R, Bartels, Robert E, Biedron, Robert R

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Economical Unsteady High-Fidelity Aerodynamics for Structural Optimization with a Flutter Constraint von Bartels, Robert E., Stanford, Bret K.

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Performance Enhancement of the Flexible Transonic Truss-Braced Wing Aircraft Using Variable-Camber Continuous Trailing-Edge Flaps von Bartels, Robert E., Stanford, Bret K., Waite, Josiah M.

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A time integration algorithm based on the state transition matrix for structures with time varying and nonlinear properties von Bartels, Robert E

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Developing an Accurate CFD Based Gust Model for the Truss Braced Wing Aircraft von Bartels, Robert E.

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Active Flutter Suppression Using Reduced-Order Modeling for Transonic Aeroservoelastic Control Law Development von Waite, Josiah M., Stanford, Bret K., Bartels, Robert E., Silva, Walter A.

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Uncertainty Due to Unsteady Fluid/Structure Interaction for the Ares I Vehicle Traversing the Transonic Regime von Bartels, Robert E.

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Reduced Order Modeling for Transonic Aeroservoelastic Control Law Development von Waite, Josiah M., Stanford, Bret K., Silva, Walter A., Bartels, Robert E.

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Active Flutter Suppression Controllers Derived from Linear and Nonlinear Aerodynamics: Application to a Transport Aircraft Model von Waite, Josiah M., Stanford, Bret K., Bartels, Robert E., Silva, Walter A., Massey, Steven J.

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