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Transitional Boundary Layer Shock Wave Interactions
Z.M. Murphree, K.B. Yuceil, N.T. Clemens, and D.S. Dolling
Physics and Control of Unstart in Supersonic Inlets and Isolators
J. L. Wagner, A. Valdivia, K. B. Yuceil, N.T. Clemens, D. S. Dolling
Supersonic flow control using plasma actuators
J. Shin, V. Narayanaswamy, L. L. Raja, N. T. Clemens
Buoyancy effects in turbulent jet-flames in a crossflow
I.G. Boxx, C.A. Idicheria and N.T. Clemens
Turbulent Non-premixed Jet-flames in Normal and Low-Gravity
C.A. Idicheria, I.G. Boxx and N.T. Clemens
Investigation of unsteadiness of shock-induced separated flows
Y.X. Hou, P.C. Bueno, R.G. Austin, S.J. Beresh, M. Comninos, S.C. Chan, N.T. Clemens and D.S. Dolling
Planar laser imaging of high-speed cavity flow dynamics
O.H. Unalmis, P.C. Bueno and N.T. Clemens, and D.S. Dolling
Effects of Upstream Boundary Layer on the Unsteadiness of Shock Induced Separation, Ganapathisubramani, B., Clemens, N.T. and Dolling, D.S., Journal of Fluid Mechanics, Vol. 585, pp. 369-394, 2007.
Planar Imaging Measurements to Study the Effect of Spanwise Structure of Upstream Turbulent Boundary Layer on Shock Induced Separation, B. Ganapathisubramani, N.T. Clemens, and D.S. Dolling, AIAA-2006-324, 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada January 2006.
Experimental Studies of Transitional Boundary Layer Shock Wave Interactions, Z.R. Murphree, J. Jagodzinski, E.S.Hood, Jr., N.T. Clemens, and D.S. Dolling, AIAA-2006-326-768, 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada, January 2006.
Characterization of a Direct-Current Glow Discharge Plasma Actuator in Low-Pressure Supersonic Flow," J. Shin, V. Narayanaswamy, L.L. Raja, N.T. Clemens, AIAA Journal, Vol. 45, No. 7, pp. 1596-1605, 2007