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A Design Methodology for Rapid Implementation of Active Control Systems Across Lean Direct Injection Combustor PlatformsThe VACCG team is comprised of engineers at Virginia Tech who specialize in the subject areas of combustion physics, chemical kinetics, dynamics and controls, and signal processing. Currently, the team's work on this NRA research grant is designed to determine key factors that influence combustion control performance through a blend of theoretical and experimental investigations targeting design and demonstration of active control for three different combustors. To validiate the accuracy of conclusions about control effectiveness, a sequence of experimental verifications on increasingly complex lean, direct injection combustors is underway. During the work period January 1, 2002 through October 15, 2002, work has focused on two different laboratory-scale combustors that allow access for a wide variety of measurements. As the grant work proceeds, one key goal will be to obtain certain knowledge about a particular combustor process using a minimum of sophisticated measurements, due to the practical limitations of measurements on full-scale combustors. In the second year, results obtained in the first year will be validated on test combustors to be identified in the first quarter of that year. In the third year, it is proposed to validate the results at more realistic pressure and power levels by utilizing the facilities at the Glenn Research Center.
Document ID
20030054519
Acquisition Source
Headquarters
Document Type
Contractor Report (CR)
Authors
Baumann, William T.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Saunders, William R.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Vandsburger, Uri
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Saus, Joseph
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
April 1, 2003
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2003-212197
NAS 1.26:212197
E-13800
Report Number: NASA/CR-2003-212197
Report Number: NAS 1.26:212197
Report Number: E-13800
Funding Number(s)
CONTRACT_GRANT: NAG3-2687
WORK_UNIT: WU-708-87-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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