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Garth Hobson
Garth Hobson
Professor of Mechanical and Aerospace Engineering, Naval Postgraduate School
Verified email at nps.edu
Title
Cited by
Cited by
Year
Effects of Reynolds number and surface roughness magnitude and location on compressor cascade performance
SC Back, GV Hobson, SJ Song, KT Millsaps
592012
Inlet turbulence distortion and viscous flow development in a controlled-diffusion compressor cascade at very high incidence
GV Hobson, RP Shreeve
Journal of Propulsion and Power 9 (3), 397-404, 1993
441993
Effect of Reynolds number on separation bubbles on compressor blades in cascade
GV Hobson, DJ Hansen, DG Schnorenberg, DV Grove
Journal of Propulsion and Power 17 (1), 154-162, 2001
402001
Impact of nonuniform leading edge coatings on the aerodynamic performance of compressor airfoils
ME Elmstrom, KT Millsaps, GV Hobson, JS Patterson
262011
Experimental investigation during stall and surge in a transonic fan stage and rotor-only configuration
AJ Gannon, GV Hobson, RP Shreeve, IJ Villescas
Turbo Expo: Power for Land, Sea, and Air 4241, 367-376, 2006
232006
Prediction of cascade performance using an incompressible Navier–Stokes technique
GV Hobson, B Lakshminarayana
211991
Effect of leading edge roughness and Reynolds number on compressor profile loss
JH Im, JH Shin, GV Hobson, SJ Song, KT Millsaps
Turbo Expo: Power for Land, Sea, and Air 55225, V06AT35A034, 2013
182013
Prediction of a laminar separation bubble over a controlled-diffusion compressor blade
GV Hobson, S Weber
Turbo Expo: Power for Land, Sea, and Air 78569, V003T01A081, 2000
182000
A Transonic Compressor Stage: Part 1—Experimental Results
AJ Gannon, GV Hobson, RP Shreeve
Turbo Expo: Power for Land, Sea, and Air 41707, 571-577, 2004
172004
Spacecraft robotics toolkit: an open-source simulator for spacecraft robotic arm dynamic modeling and control
J Virgili-Llop, DV Drew, M Romano, GV Hobson, BE Wakefield, ...
6th International Conference on Astrodynamics Tools and Techniques, 2016
152016
Investigation and prediction of steam-induced stall-margin reduction in two transonic rotor fans
AJ Gannon, GV Hobson, CR Hedges, GL Descovich
Journal of Fluids Engineering 136 (11), 111101, 2014
142014
Pre-stall instability distribution over a transonic compressor rotor
AJ Gannon, GV Hobson
142009
The effect of steam ingestion on transonic rotor stall margin
AJ Gannon, GV Hobson, TA Payne, SE Zarro
Turbo Expo: Power for Land, Sea, and Air 47950, 389-398, 2007
132007
Steady state and transient measurements within a compressor rotor during steam-induced stall at transonic operational speeds
SE Zarro, GV Hobson
Naval Postgraduate School, 2006
132006
Computation of turbine flowfields with a Navier-Stokes code
G Hobson, B Lakshminarayana
26th Joint Propulsion Conference, 2122, 1990
131990
Microstructural Study of IF-WS2 Failure Modes
J Cook, S Rhyans, L Roncase, G Hobson, CC Luhrs
Inorganics 2 (3), 377-395, 2014
122014
Performance of a ducted micro-turbojet engine
L Andreou
Monterey, California: Naval Postgraduate School, 1999
121999
Numerical and experimental investigation of low Reynolds number effects on laminar flow separation and transition in a cascade of compressor blades
S Enomoto, C Hah, GV Hobson
Turbo Expo: Power for Land, Sea, and Air 78569, V003T01A080, 2000
112000
Effect of surface roughness location and reynolds number on compressor cascade performance
SC Back, GV Hobson, SJ Song, KT Millsaps
Turbo Expo: Power for Land, Sea, and Air 44021, 121-128, 2010
102010
Pre-stall modal instabilities in a transonic compressor rotor
AJ Gannon, GV Hobson
Proc. 18th ISABE, 2007
102007
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