Claude G. Matalanis, Ph.D. - Publications

Affiliations: 
2007 Stanford University, Palo Alto, CA 
Area:
Mechanical Engineering, Aerospace Engineering

8 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2017 Matalanis CG, Bowles PO, Min B, Jee S, Kuczek AE, Wake BE, Lorber PF, Crittenden TM, Glezer A, Schaeffler NW. High-Speed Experiments on Combustion-Powered Actuation for Dynamic Stall Suppression Aiaa Journal. 55: 3001-3015. DOI: 10.2514/1.J055700  0.44
2015 Matalanis CG, Min BY, Bowles PO, Jee S, Wake BE, Crittenden TM, Woo G, Glezer A. Combustion-powered actuation for dynamic-stall suppression: High-Mach simulations and low-Mach experiments Aiaa Journal. 53: 2151-2163. DOI: 10.2514/1.J053641  0.455
2012 Florea RV, Matalanis C, Hardin LW, Stucky M, Shabbir A. Parametric analysis and design for embedded engine inlets 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012. DOI: 10.2514/1.B34804  0.399
2011 Matalanis CG, Wake BE, Opoku D, Min BY, Yeshala N, Sankar L. Aerodynamic evaluation of miniature trailing-edge effectors for active rotor control Journal of Aircraft. 48: 995-1004. DOI: 10.2514/1.C031191  0.526
2008 Chen Y, Matalanis CG, Eaton JK. High resolution PIV measurements around a model turbine blade trailing edge film-cooling breakout Experiments in Fluids. 44: 199-209. DOI: 10.1007/S00348-007-0391-2  0.498
2007 Matalanis CG, Nelson GD, Eaton JK. Novel aerodynamic device for wake vortex alleviation Aiaa Journal. 45: 2350-2352. DOI: 10.2514/1.30124  0.551
2007 Matalanis CG, Eaton JK. Wake vortex alleviation using rapidly actuated segmented gurney flaps Aiaa Journal. 45: 1874-1884. DOI: 10.2514/1.28319  0.601
2007 Matalanis CG, Eaton JK. Wake vortex control using static segmented gurney flaps Aiaa Journal. 45: 321-328. DOI: 10.2514/1.25956  0.605
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