An Overview Of High Bandwidth Liquid Fuel Flow Modulators Developed For Active Combustion Control Research
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Author | : |
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Total Pages | : 488 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
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Total Pages | : 974 |
Release | : 1999 |
Genre | : Aeronautics |
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Author | : North Atlantic Treaty Organization. Research and Technology Organization. Applied Vehicle Technology Panel. Symposium |
Publisher | : |
Total Pages | : 622 |
Release | : 1999 |
Genre | : Aircraft exhaust emissions |
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The symposium dealt with Gas Turbine Engine Combustion, Emissions and Alternative Fuels. Forty-six papers and a Keynote Address elucidated the role of the combustion process as a crucial factor of engine performance and operability under various conditions including non-standard, new fuels and environmental effects of civil and military interest. There were 12 Sessions covering the following topics (some in 2 sessions): (1) Gas Turbines in Land, Sea and Air Applications; (2) Low-Emission Combustors; (3) Combustion Modelling; (4) Optical Measurements; (5) Emissions; (6) Combustor Design; (7) Ignition Processes; (8) Active Combustion Control; and (9) Alternative Fuels.
Author | : Dr. Kuehn |
Publisher | : |
Total Pages | : 784 |
Release | : 1925 |
Genre | : Atomization |
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Author | : |
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Total Pages | : 654 |
Release | : 1992 |
Genre | : Aeronautics |
ISBN | : |
Author | : |
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Total Pages | : 418 |
Release | : 2000 |
Genre | : Mechanical engineering |
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Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 26 |
Release | : 2018-05-22 |
Genre | : |
ISBN | : 9781719390651 |
At the NASA Glenn Research Center, a characterization rig was designed and constructed for the purpose of evaluating high bandwidth liquid fuel modulation devices to determine their suitability for active combustion control research. Incorporated into the rig s design are features that approximate conditions similar to those that would be encountered by a candidate device if it were installed on an actual combustion research rig. The characterized dynamic performance measures obtained through testing in the rig are planned to be accurate indicators of expected performance in an actual combustion testing environment. To evaluate how well the characterization rig predicts fuel modulator dynamic performance, characterization rig data was compared with performance data for a fuel modulator candidate when the candidate was in operation during combustion testing. Specifically, the nominal and off-nominal performance data for a magnetostrictive-actuated proportional fuel modulation valve is described. Valve performance data were collected with the characterization rig configured to emulate two different combustion rig fuel feed systems. Fuel mass flows and pressures, fuel feed line lengths, and fuel injector orifice size was approximated in the characterization rig. Valve performance data were also collected with the valve modulating the fuel into the two combustor rigs. Comparison of the predicted and actual valve performance data show that when the valve is operated near its design condition the characterization rig can appropriately predict the installed performance of the valve. Improvements to the characterization rig and accompanying modeling activities are underway to more accurately predict performance, especially for the devices under development to modulate fuel into the much smaller fuel injectors anticipated in future lean-burning low-emissions aircraft engine combustors. Saus, Joseph R. and DeLaat, John C. and Chang, Clarence T. and Vrnak, Daniel R. Glenn Research Center COMBUSTION CONTROL; ACTIVE CONTROL; FUEL SYSTEMS; PERFORMANCE TESTS; MAGNETOSTRICTION; BANDWIDTH; FUEL INJECTION; FEED SYSTEMS; COMBUSTION CHAMBERS; MASS FLOW; MODULATORS
Author | : |
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Total Pages | : 654 |
Release | : 1997 |
Genre | : Aeronautics |
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Author | : Arthur H. Lefebvre |
Publisher | : CRC Press |
Total Pages | : 284 |
Release | : 2017-03-27 |
Genre | : Technology & Engineering |
ISBN | : 1498736262 |
The second edition of this long-time bestseller provides a framework for designing and understanding sprays for a wide array of engineering applications. The text contains correlations and design tools that can be easily understood and used in relating the design of atomizers to the resulting spray behavior. Written to be accessible to readers with a modest technical background, the emphasis is on application rather than in-depth theory. Numerous examples are provided to serve as starting points for using the information in the book. Overall, this is a thoroughly updated edition that still retains the practical focus and readability of the original work by Arthur Lefebvre.
Author | : |
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Total Pages | : 410 |
Release | : 1988 |
Genre | : Power resources |
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