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Computational Three-Dimensional Flapping-Wing AnalysisBUCHMANN, Nadine; RADESPIEL, Rolf.AIAA journal. 2014, Vol 52, Num 1, pp 203-206, issn 0001-1452, 4 p.Article

Computing the Effects of Practical Tolerances on Propellant Management Device PerformanceCOLLICOTT, Steven H.AIAA journal. 2014, Vol 52, Num 7, pp 1578-1580, issn 0001-1452, 3 p.Article

Measurement of Unsteady Flow Reattachment on an Airfoil with an Ice ShapeANSELL, Phillip J; BRAGG, Michael B.AIAA journal. 2014, Vol 52, Num 3, pp 656-659, issn 0001-1452, 4 p.Article

Mirror-Based Image Derotation for Aerodynamic Rotor MeasurementsRAFFEL, Markus; HEINECK, James T.AIAA journal. 2014, Vol 52, Num 6, pp 1337-1341, issn 0001-1452, 5 p.Article

Efficient Global Optimization with Adaptive Target SettingCHAUDHURI, Anirban; HAFTKA, Raphael T.AIAA journal. 2014, Vol 52, Num 7, pp 1573-1578, issn 0001-1452, 6 p.Article

Membrane Paradox for Solar SailsCHAD GIBBS, S; DOWELL, Earl H.AIAA journal. 2014, Vol 52, Num 12, pp 2904-2907, issn 0001-1452, 4 p.Article

Rocket Plume ModelingCHUNPEI CAI.AIAA journal. 2014, Vol 52, Num 12, pp 2907-2910, issn 0001-1452, 4 p.Article

Computational Study on Hysteretic Inlet Buzz Characteristics Under Varying Mass Flow ConditionsWOORAM HONG; CHONGAM KIM.AIAA journal. 2014, Vol 52, Num 7, pp 1357-1373, issn 0001-1452, 17 p.Article

Dynamic Stall Modeling for the Conditions of Vertical Axis Wind TurbinesDYACHUK, Eduard; GOUDE, Anders; BERNHOFF, Hans et al.AIAA journal. 2014, Vol 52, Num 1, pp 72-81, issn 0001-1452, 10 p.Article

Flat-Plate Drag Reduction with Streamwise Noncontinuous MicroblowingKORNILOV, Vladimir I; BOIKO, Andrey V.AIAA journal. 2014, Vol 52, Num 1, pp 93-103, issn 0001-1452, 11 p.Article

High-Altitude Gas Balloon Trajectory Prediction: A Monte Carlo ModelSOBESTER, András; CZERSKI, Helen; ZAPPONI, Niccolò et al.AIAA journal. 2014, Vol 52, Num 4, pp 832-842, issn 0001-1452, 11 p.Article

Intuitive Class/Shape Function Parameterization for AirfoilsFENG ZHU; NING QIN.AIAA journal. 2014, Vol 52, Num 1, pp 17-25, issn 0001-1452, 9 p.Article

New Adaptive Technique of Kirsch Method for Structural ReanalysisRUIHENG SUN; DAYOU LIU; TAO XU et al.AIAA journal. 2014, Vol 52, Num 3, pp 486-495, issn 0001-1452, 10 p.Article

Spectral Power Iterations for the Random Eigenvalue ProblemMEIDANI, Hadi; GHANEM, Roger.AIAA journal. 2014, Vol 52, Num 5, pp 912-925, issn 0001-1452, 14 p.Article

Supersonic Natural-Laminar-Flow Wing-Design Concept at High-Reynolds-Number ConditionsUEDA, Yoshine; YOSHIDA, Kenji; MATSUSHIMA, Kisa et al.AIAA journal. 2014, Vol 52, Num 6, pp 1294-1306, issn 0001-1452, 13 p.Article

Time-Domain Harmonic Balance Method for Turbomachinery AeroelasticitySICOT, Frédéric; GOMAR, Adrien; DUFOUR, Guillaume et al.AIAA journal. 2014, Vol 52, Num 1, pp 62-71, issn 0001-1452, 10 p.Article

Vibration Suppression in a Simple Tension-Aligned Array StructureCAI, Tingli; MUKHERJEE, Ranjan; DIAZ, Alejandro R et al.AIAA journal. 2014, Vol 52, Num 3, pp 504-515, issn 0001-1452, 12 p.Article

Deformation Measurement of a Birdlike Airfoil with Optical Flow and Numerical SimulationXIAOLIANG GONG; BANSMER, Stephan; STROBACH, Christoph et al.AIAA journal. 2014, Vol 52, Num 12, pp 2807-2816, issn 0001-1452, 10 p.Article

Effects of a Free-to-Roll Fuselage on Wing Flutter: Theory and ExperimentTANG, Deman; DOWELL, Earl H.AIAA journal. 2014, Vol 52, Num 12, pp 2625-2632, issn 0001-1452, 8 p.Article

Improvement of Corner Flow Prediction Using the Quadratic Constitutive RelationDANDOIS, Julien.AIAA journal. 2014, Vol 52, Num 12, pp 2795-2806, issn 0001-1452, 12 p.Article

Investigation of Hypersonic Intakes Using Reynolds Stress Modeling and Wavelet-Based AdaptationFRAUHOLZ, Sarah; BOSCO, Arianna; REINARTZ, Birgit U et al.AIAA journal. 2014, Vol 52, Num 12, pp 2765-2781, issn 0001-1452, 17 p.Article

Multiple-Fidelity Computational Framework for the Design of Efficient Flapping WingsWILLIS, David J; PERSSON, Per-Olof.AIAA journal. 2014, Vol 52, Num 12, pp 2840-2854, issn 0001-1452, 15 p.Article

Simplified Theory for Hygrothermal Response of Angle-Ply Composite PlatesZENKOUR, Ashraf M.AIAA journal. 2014, Vol 52, Num 7, pp 1466-1473, issn 0001-1452, 8 p.Article

Unsteady Aerodynamic Modeling of Aircraft Control Surfaces by Indicial Response MethodsGHOREYSHI, Mehdi; CUMMINGS, Russell M.AIAA journal. 2014, Vol 52, Num 12, pp 2683-2700, issn 0001-1452, 18 p.Article

Zonal Immersed Boundary Conditions: Application to a High-Reynolds-Number Afterbody FlowMOCHEL, Loïc; WEISS, Pierre-Elie; DECK, Sébastien et al.AIAA journal. 2014, Vol 52, Num 12, pp 2782-2794, issn 0001-1452, 13 p.Article

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