High-Speed Experiments on Combustion-Powered Actuation for Dynamic Stall Suppression von Matalanis, Claude G, Bowles, Patrick O, Min, Byung-Young, Jee, Solkeun, Kuczek, Andrzej E, Wake, Brian E, Lorber, Peter F, Crittenden, Thomas M, Glezer, Ari, Schaeffler, Norman W

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Experimental Investigation of Separation Control Part 1: Baseline and Steady Suction von Greenblatt, David, Paschal, Keith B, Yao, Chung-Sheng, Harris, Jerome, Schaeffler, Norman W, Washburn, Anthony E

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Isolated Synthetic Jet in Crossflow: Experimental Protocols for a Validation Dataset von Schaeffler, Norman W, Jenkins, Luther N

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Active Control of Flow Separation from Supercritical Airfoil Leading-Edge Flap Shoulder von Melton, LaTunia Pack, Schaeffler, Norman W, Yao, Chung-Sheng, Seifert, Avi

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Hover Validation and Acoustic Baseline Blade Set von Overmeyer, Austin D, Copp, Peter A, Schaeffler, Norman W

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Numerical Investigation of Rotorcraft Fuselage Drag Reduction Using Active Flow Control von Allan, Brian G., Schaeffler, Norman W.

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Active Aerodynamic Load Reduction on a Rotorcraft Fuselage With Rotor Effects: A CFD Validation Effort von Allan, Brian G., Schaeffler, Norman W., Jenkins, Luther N., Yao, Chung-Sheng, Wong, Oliver D., Tanner, Philip E.

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Mechanisms of Active Aerodynamic Load Reduction on a Rotorcraft Fuselage With Rotor Effects von Schaeffler, Norman W., Allan, Brian G., Jenkins, Luther N., Yao, Chung-Sheng, Bartram, Scott M., Mace, W. Derry, Wong, Oliver D., Tanner, Philip E.

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Overview of active flow control actuator development at NASA langley research center von Schaeffler, Norman W, Hepner, Timothy E, Jones, Gregory S, Kegerise, Michael A

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Active control of separation from the slat shoulder of a supercritical airfoil von Pack, La Tunia G, Schaeffler, Norman W, Yao, Chung-Sheng, Seifert, Avi

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Progress Towards Fuselage Drag Reduction via Active Flow Control: A Combined CFD and Experimental Effort von Schaeffler, Norman W., Allan, Brian G., Lienard, Caroline, LePape, Arnaud

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RVLT Validation Test Plan von Schaeffler, Norman W

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Experimental Evaluation of an Isolated Synthetic Jet IN Crossflow von Schaeffler, Norman W., Jenkins, Luther N., Hepner, Timothy E.

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High-Lift System for a Supercritical Airfoil: Simplified by Active Flow Control von Melton, LaTunia Pack, Schaeffler, Norman W., Lin, John C.

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The Isolated Synthetic Jet in Crossflow: A Benchmark for Flow Control Simulation von Schaeffler, Norman W., Jenkins, Luther N.

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The Isolated Synthetic Jet in Crossflow: A Benchmark for Flow Control Simulation von Schaeffler, Norman W., Jenkins, Luther N.

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Time-Accurate Computations of Isolated Circular Synthetic Jets in Crossflow von Rumsey, Christoper L., Schaeffler, Norman W., Milanovic, I. M., Zaman, K. B. M. Q.

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A Separation Control CFD Validation Test Case von Greenblatt, David, Paschal, Keith B., Yao, Chung-Sheng, Harris, jerome, Schaeffler, Norman W., Washburn, Anthony E.

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Active Control of Separation from the Slat Shoulder of a Supercritical Airfoil von Pack, LaTunia G., Schaeffler, Norman W., Yao, Chung-Sheng, Seifert, Avi

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Fundamental Test of a Hovering Rotor: Comprehensive Measurements for CFD Validation von Norman, Thomas R, Heineck, James T, Schairer, Edward T, Schaeffler, Norman W, Wagner, Lauren N, Yamauchi, Gloria K, Overmeyer, Austin D, Ramasamy, Manikandan, Cameron, Christopher G, Dominguez, Michelle, Sheikman, Alex

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