Garth V. Hobson

Effects of Reynolds Number and Surface Roughness Magnitude and Location on Compressor Cascade Performance

Seung Chul Back, Garth V. Hobson, Seung Jin Song et al. · Journal of Turbomachinery · 2012 · 47 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Effect of Reynolds Number on Separation Bubbles on Compressor Blades in Cascade

Garth V. Hobson, Denis J. Hansen, David G. Schnorenberg et al. · Journal of Propulsion and Power · 2001 · 29 citations

Engineering, Aerospace Engineering, Physics +17

Impact of Nonuniform Leading Edge Coatings on the Aerodynamic Performance of Compressor Airfoils

Michael E. Elmstrom, Knox Millsaps, Garth V. Hobson et al. · Journal of Turbomachinery · 2011 · 22 citations

Engineering, Aerospace Engineering, Computational Engineering +17

Inlet turbulence distortion and viscous flow development in a controlled-diffusion compressor cascade at very high incidence

Garth V. Hobson, R. P. Shreeve · Journal of Propulsion and Power · 1993 · 19 citations

Natural Sciences, Aerospace Engineering, Aerodynamics +15

Effect of Leading Edge Roughness and Reynolds Number on Compressor Profile Loss

Ju Hyun Im, Ju Hyun Shin, Garth V. Hobson et al. · 2013 · 15 citations

Engineering, Aerospace Engineering, Aerodynamics +16