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2017, 1, ISBN 9780415620987, Volume 14, 396
Aircraft emissions currently account for ~3.5% of all greenhouse gas emissions. The number of passenger miles has increased by 5% annually despite 9/11, two... 
Aerospace Engineering | Pollution | Energy | Traditional Industries - Clean & Green Advancements
eBook
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
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, 2012
Conference Proceeding
Annual Forum Proceedings - AHS International, ISSN 1552-2938, 2018, Volume 2018-
Conference Proceeding
07/2012
The NASA Environmentally Responsible Aviation (ERA) Project is focused on developing and demonstrating integrated systems technologies to TRL 4-6 by 2020 that... 
Aircraft Propulsion and Power
Conference Proceeding
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
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
2017, 1, ISBN 0415620988, Volume 14
This chapter focuses on aerothermodynamic improvements to aircraft engine systems that were enabled through National Aeronautics and Space Administration... 
Book Chapter
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009
Conference Proceeding
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, 2013
Conference Proceeding
Proceedings of the ASME Turbo Expo, 2010, Volume 7, Issue C, pp. 465 - 475
Conference Proceeding
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
Proceedings of the ASME Turbo Expo, 2010, Volume 7, Issue C, pp. 329 - 342
Conference Proceeding
10/2009
The propulsion research portfolio of the National Aeronautics and Space Administration Fundamental Aeronautics Program Hypersonics Project encompasses a... 
Fluid Mechanics and Thermodynamics
Conference Proceeding
10/2007
NASA s Fundamental Aeronautics Program is investigating turbine-based propulsion systems for access to space because it provides the potential for... 
Aircraft Propulsion and Power
Report
Proceedings of the ASME Turbo Expo 2004, 2004, Volume 5, pp. 655 - 667
Conference Proceeding
10/2010
NASA and GE teamed to design and build a 57 percent engine scaled fan stage for a Mach 4 variable cycle turbofan/ramjet engine for access to space with... 
Fluid Mechanics and Thermodynamics
Report
10/2011
NASA s Fundamental Aeronautics Program is investigating turbine-based combined cycle (TBCC) propulsion systems for access to space because it provides the... 
Aerodynamics
Report
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