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Journal of Turbomachinery, ISSN 0889-504X, 2015, Volume 137, Issue 5
Numerical prediction of the Stage 67 transonic fan stage employing wall jet tip injection flow control and study of the physical mechanisms leading to stall... 
ENGINEERING, MECHANICAL | Fans | Stalling (Aerodynamics) | Control | Usage | Reynolds number | Mechanical properties | Navier-Stokes equations | Spikes | Harmonics | NASA | Stall | Nonlinearity | Mathematical models | Walls | Engineering
Journal Article
Journal of Turbomachinery, ISSN 0889-504X, 10/2012, Volume 135, Issue 1, pp. 1 - 6
Back-to-back testing was done using NASA fan rotor 67 in the Glenn Research Center W8 Axial Compressor Test Facility. The rotor was baseline tested with a... 
ENGINEERING, MECHANICAL | Dynamic testing | Rotors | Research | Properties | Finishes and finishing | Methods | Testing | Surface finish | Test facilities | Error analysis | Blades | NASA | Compressors | Mach number
Journal Article
Journal of Turbomachinery, ISSN 0889-504X, 01/2001, Volume 123, Issue 1, pp. 14 - 23
Mass injection upstream of the tip of a high-speed axial compressor rotor is a stability enhancement approach known to be effective in suppressing stall in... 
SPEED AXIAL COMPRESSOR | ACTIVE STABILIZATION | CLEARANCE | ROTOR | FAN | STAGE | SURGE | ROTATING STALL CONTROL | FLOW | ENGINEERING, MECHANICAL | INLET DISTORTION | Turbofan engines | Compressors | Design and construction | Airplanes, Military | Turbomachines
Journal Article
Journal of Turbomachinery, ISSN 0889-504X, 2000, Volume 122, Issue 4, pp. 733 - 742
The tip clearance flows of transonic compressor rotors are important because they have a significant impact on rotor and stage performance. A wall-bounded... 
3-DIMENSIONAL VISCOUS-FLOW | ENGINEERING, MECHANICAL | Turbomachines | Turbines | Research
Journal Article
Journal of Turbomachinery, ISSN 0889-504X, 01/2004, Volume 126, Issue 1, pp. 24 - 34
Active flow control has been applied to the suction surface of stator vanes in a low speed axial compressor Injection from the suction surface has been shown... 
ENGINEERING, MECHANICAL | Turbomachines | Research
Journal Article
Journal of Turbomachinery, ISSN 0889-504X, 04/2002, Volume 124, Issue 2, pp. 275 - 284
Rotor wakes are an important source of loss in axial compressors. The decay rate of a rotor wake is largely due to both mixing (results in loss) and stretching... 
ENGINEERING, MECHANICAL | Aerodynamics | Compressors | Research | Wakes (Aerodynamics) | Dynamics | Rotors
Journal Article
STAR, ISSN 1548-8837, 11/2006, Volume 44, Issue 22
An endwall treatment for a gas turbine engine having at least one rotor blade extending from a rotatable hub and a casing circumferentially surrounding the... 
Journal Article
STAR, ISSN 1548-8837, 02/2003, Volume 41, Issue 4
Aircraft fan and compressor blade leading edges suffer from atmospheric particulate erosion that reduces aerodynamic performance. Recontouring the blade... 
Journal Article
Journal of Turbomachinery, ISSN 0889-504X, 07/2002, Volume 124, Issue 3, pp. 351 - 357
Aircraft fan and compressor blade leading edges suffer from atmospheric particulate erosion that reduces aerodynamic performance. Recontouring the blade... 
Performance restoration | Variable chord | Blade recontour | Axial compressor | variable chord | axial compressor | blade recontour | ENGINEERING, MECHANICAL | performance restoration | Aerodynamics | Research | Dynamics | Turbomachines | Rotors
Journal Article
Proceedings of the ASME Turbo Expo 2004, 2004, Volume 5, pp. 655 - 667
Conference Proceeding
Journal of Engineering for Gas Turbines and Power, ISSN 0742-4795, 04/1985, Volume 107, Issue 2, pp. 427 - 435
Journal Article
American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI, 2003, Volume 6, pp. 1039 - 1050
Conference Proceeding
Journal of Turbomachinery, 07/2002, Volume 24, p. 351
Aircraft fan and compressor blade leading edges suffer from atmospheric particulate erosion that reduces aerodynamic performance. Recontouring the blade... 
Aircraft Propulsion and Power
Journal Article
The Effect of Variable Chord Length on Transonic Axial Rotor Performance, 07/2002
Aircraft fan and compressor blade leading edges suffer from atmospheric particulate erosion that reduces aerodynamic performance. Recontouring the blade... 
Journal Article
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