| Effects of Reynolds number and surface roughness magnitude and location on compressor cascade performance SC Back, GV Hobson, SJ Song, KT Millsaps | 62 | 2012 |
| 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 | 42 | 1993 |
| 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 | 41 | 2001 |
| Impact of nonuniform leading edge coatings on the aerodynamic performance of compressor airfoils ME Elmstrom, KT Millsaps, GV Hobson, JS Patterson | 27 | 2011 |
| 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 | 24 | 2006 |
| Prediction of cascade performance using an incompressible Navier–Stokes technique GV Hobson, B Lakshminarayana | 21 | 1991 |
| 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 | 20 | 2013 |
| Design, test, and evaluation of a transonic axial compressor rotor with splitter blades S Drayton, GV Hobson Monterey, California: Naval Postgraduate School, 2013 | 19 | 2013 |
| 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 | 18 | 2000 |
| 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 | 17 | 2016 |
| 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 | 17 | 2004 |
| 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 | 15 | 2014 |
| Pre-stall instability distribution over a transonic compressor rotor AJ Gannon, GV Hobson | 14 | 2009 |
| Computation of turbine flowfields with a Navier-Stokes code G Hobson, B Lakshminarayana 26th Joint Propulsion Conference, 2122, 1990 | 14 | 1990 |
| 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 | 13 | 2007 |
| 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 | 13 | 2006 |
| 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 | 13 | 2000 |
| Microstructural Study of IF-WS2 Failure Modes J Cook, S Rhyans, L Roncase, G Hobson, CC Luhrs Inorganics 2 (3), 377-395, 2014 | 12 | 2014 |
| Performance of a ducted micro-turbojet engine L Andreou Monterey, California: Naval Postgraduate School, 1999 | 12 | 1999 |
| Impact of Non-uniform leading edge coatings on the aerodynamic performance of compressor airfoils ME Elmstrom, KT Millsaps, GV Hobson, JS Patterson Turbo Expo: Power for Land, Sea, and Air 47306, 103-113, 2005 | 11 | 2005 |
Anthony J GannonResearch Associate Prof. Naval Postgraduate SchoolVerified email at nps.edu
