G. Paniagua

Starting Mechanisms For High Contraction Ratio Hypersonic Inlets

Sebastien Paris, A. L. Grainger, Sc. Tirtey, 2011 .

Pulsating Cooling System for High Pressure Turbine Blades

M. Gonz, G. Paniagua, B. Saraço, 2010 .

Design of the Purdue Experimental Turbine Aerothermal Laboratory for Optical and Surface Aerothermal Measurements

Guillermo Paniagua, Scott E. Meyer, Jorge Saavedra, 2016, Journal of Engineering for Gas Turbines and Power.

Effect of the hub endwall cavity flow on the flow-field of a transonic high-pressure turbine

R. Dénos, G. Paniagua, S. Almeida, 2004 .

Enhanced performance of fast-response 3-hole wedge probes for transonic flows in axial turbomachinery

R. Dénos, D. Delhaye, G. Paniagua, 2011 .

Effect of the Hub Endwall Cavity Flow on the Flow-Field of a Transonic High-Pressure Turbine (2004-GT-53458)

G. Paniagua, 2004 .

Modeling, Analysis, and Optimization of theAir-Turborocket Expander Engine

G. Paniagua, G. Paniagua, I. Rodríguez-Miranda, 2013 .

Characterization of a Supersonic Turbine Downstream of a Rotating Detonation Combustor

G. Paniagua, Zhe Liu, G. Paniagua, 2018, Journal of Engineering for Gas Turbines and Power.