Impulsively Started Flat Plate CirculationPITT FORD, Charles W; BABINSKY, Holger.AIAA journal. 2014, Vol 52, Num 8, pp 1800-1802, issn 0001-1452, 3 p.Article

Prediction of Lift Cells for Stalling Wings by Lifting-Line TheorySPALART, Philippe R.AIAA journal. 2014, Vol 52, Num 8, pp 1817-1821, issn 0001-1452, 5 p.Article

Compressible dynamic stall control using high momentum microjetsBEAHAN, James J; CHIANG SHIH; KROTHAPALLI, Anjaneyulu et al.Experiments in fluids. 2014, Vol 55, Num 9, issn 0723-4864, 1813.1-1813.11Article

Experimental study of flow separation control on a low-Re airfoil using leading-edge protuberance methodZHANG, M. M; WANG, G. F; XU, J. Z et al.Experiments in fluids. 2014, Vol 55, Num 4, issn 0723-4864, 1710.1-1710.13Article

Flow structure on a rotating wing: effect of radius of gyrationWOLFINGER, M; ROCKWELL, D.Journal of fluid mechanics. 2014, Vol 755, pp 83-110, issn 0022-1120, 28 p.Article

Investigation of three-dimensional dynamic stall on an airfoil using fast-response pressure-sensitive paintGARDNER, A. D; KLEIN, C; SACHS, W. E et al.Experiments in fluids. 2014, Vol 55, Num 9, issn 0723-4864, 1807.1-1807.14Article

Kriging regression of PIV data using a local error estimateDE BAAR, Jouke H. S; PERCIN, Mustafa; DWIGHT, Richard P et al.Experiments in fluids. 2014, Vol 55, Num 1, issn 0723-4864, 1650.1-1650.13Article

Low-Reynolds-number effect on the aerodynamic characteristics of a pitching NACA0012 airfoilKIM, Dong-Ha; CHANG, Jo-Won.Aerospace science and technology (Imprimé). 2014, Vol 32, pp 162-168, issn 1270-9638, 7 p.Article

On the use of synthetic jet actuator arrays for active flow separation controlHUI TANG; SALUNKHE, Pramod; YINGYING ZHENG et al.Experimental thermal and fluid science. 2014, Vol 57, pp 1-10, issn 0894-1777, 10 p.Article

Reduced-Order Modeling of Steady Flows Subject to Aerodynamic ConstraintsZIMMERMANN, Ralf; VENDL, Alexander; GÖRTZ, Stefan et al.AIAA journal. 2014, Vol 52, Num 2, pp 255-266, issn 0001-1452, 12 p.Article

Velocity measurements on a retreating blade in dynamic stallRAGHAV, Vrishank; KOMERATH, Narayanan.Experiments in fluids. 2014, Vol 55, Num 2, issn 0723-4864, 1669.1-1669.10Article

Discrete Vortex Method-Based Model for Ground-Effect StudiesMONDAL, Partha; BALAKRISHNAN, N.AIAA journal. 2014, Vol 52, Num 12, pp 2817-2828, issn 0001-1452, 12 p.Article

Inverse airfoil design using variable-resolution models and shape-preserving response predictionLEIFSSON, Leifur; KOZIEL, Slawomir.Aerospace science and technology (Imprimé). 2014, Vol 39, pp 513-522, issn 1270-9638, 10 p.Article

Unsteady aerodynamics modeling for aircraft maneuvers: A new approach using time-dependent surrogate modelingGHOREYSHI, Mehdi; CUMMINGS, Russell M.Aerospace science and technology (Imprimé). 2014, Vol 39, pp 222-242, issn 1270-9638, 21 p.Article

Comparative Study of Effects of Sweep and Humps on High-Speed Propeller BladesMARINUS, Benoît G.AIAA journal. 2014, Vol 52, Num 4, pp 739-746, issn 0001-1452, 8 p.Conference Paper

Numerical Evidence of Multiple Solutions for the Reynolds-Averaged Navier-Stokes EquationsKAMENETSKIY, Dmitry S; BUSSOLETTI, John E; HILMES, Craig L et al.AIAA journal. 2014, Vol 52, Num 8, pp 1686-1698, issn 0001-1452, 13 p.Conference Paper

Pulsed Jets Laminar Separation Control Using Instability ExploitationBERNARDINI, Chiara; BENTON, Stuart I; CHEN, Jen-Ping et al.AIAA journal. 2014, Vol 52, Num 1, pp 104-115, issn 0001-1452, 12 p.Conference Paper

Swept-Wing Boundary-Layer Transition and Turbulent Flow Physics from Multipoint MeasurementsGLAUSER, Mark N; SARIC, William S; CHAPMAN, Keith L et al.AIAA journal. 2014, Vol 52, Num 2, pp 338-347, issn 0001-1452, 10 p.Conference Paper

Active Load Control of a Wind Turbine Airfoil Using MicrotabsCOOPERMAN, Aubryn M; CHOW, Raymond; VAN DAM, C. P et al.Journal of aircraft. 2013, Vol 50, Num 4, pp 1150-1158, issn 0021-8669, 9 p.Article

Anisotropic h p-Adaptation Framework for Functional PredictionCEZE, Marco; FIDKOWSKI, Krzysztof J.AIAA journal. 2013, Vol 51, Num 2, pp 492-509, issn 0001-1452, 18 p.Article

Challenges in the aerodynamics modeling of an oscillating and translating airfoil at large incidence anglesGHOREYSHI, Mehdi; CUMMINGS, Russell M.Aerospace science and technology (Imprimé). 2013, Vol 28, Num 1, pp 176-190, issn 1270-9638, 15 p.Article

Closed-Loop Dynamic Stall Control Using a Plasma ActuatorLOMBARDI, Andrew J; BOWLES, Patrick O; CORKE, Thomas C et al.AIAA journal. 2013, Vol 51, Num 5, pp 1130-1141, issn 0001-1452, 12 p.Article

Constrained Adjoint-Based Aerodynamic Shape Optimization of a Single-Stage Transonic CompressorWALTHER, Benjamin; NADARAJAH, Siva.Journal of turbomachinery. 2013, Vol 135, Num 2, issn 0889-504X, 021017.1-021017.10Article

Derivative-Enhanced Variable Fidelity Surrogate Modeling for Aerodynamic FunctionsYAMAZAKI, Wataru; MAVRIPLIS, Dimitri J.AIAA journal. 2013, Vol 51, Num 1, pp 126-137, issn 0001-1452, 12 p.Article

Discrete Adjoint-Based Design for Unsteady Turbulent Flows on Dynamic Overset Unstructured GridsNIELSEN, Eric J; DISKIN, Boris.AIAA journal. 2013, Vol 51, Num 6, pp 1355-1373, issn 0001-1452, 19 p.Article