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American Society of Mechanical Engineers, Aerospace Division (Publication) AD, ISSN 0733-4230, 1994, Volume 40, pp. 1 - 11
Conference Proceeding
ASME, International Gas Turbine and Aeroengine Congress and Exhibition, Indianapolis, IN; UNITED STATES; 7-10 June 1999, 06/1999
The tip clearance flows of transonic compressor rotors are important because they have a significant impact on rotor and stage performance. While numerical... 
Conference Proceeding
06/2003
Micro-flow control actuation embedded in a stator vane was used to successfully control separation and improve near stall performance in a multistage... 
Aircraft Propulsion and Power
Report
ASME, International Gas Turbine and Aeroengine Congress and Exhibition, Orlando, FL; UNITED STATES; 2-5 June 1997, 06/1997
This paper addresses the significant differences in compressor rotor wake mixing loss which exist in a stage environment relative to a rotor in isolation. It... 
Conference Proceeding
Proceedings of the ASME Turbo Expo, 1997, Volume 1
Conference Proceeding
01/2001
Mass injection upstream of the tip of a high-speed axial compressor rotor is a stability enhancement approach known to be effective in suppressing small in... 
Aircraft Propulsion and Power
Report
09/2000
The tip clearance flows of transonic compressor rotors are important because they have a significant impact on rotor and stage performance. While numerical... 
Aircraft Propulsion and Power
Report
04/1998
In a joint effort between the Massachusetts Institute of Technology (MIT) and the NASA Lewis Research Center, a new technology was demonstrated to identify and... 
Aircraft Propulsion and Power
Report
03/2000
The tip clearance flows of transonic compressor rotors have a significant impact on rotor and stage performance. Although numerical simulations of these flows... 
Aircraft Propulsion and Power
Report
American Society of Mechanical Engineers (Paper), ISSN 0402-1215, 1994, pp. 1 - 20
Conference Proceeding
Proceedings of the ASME Turbo Expo, 1994, Volume 1
Conference Proceeding
01/1991
NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion research and development. Efforts are underway to develop a... 
COMPUTER SYSTEMS
Report
01/1991
NASA-Lewis has committed to a long range goal of creating a numerical test cell for aeropropulsion research and development. Efforts are underway to develop a... 
COMPUTER SYSTEMS
Report
American Society of Mechanical Engineers (Paper), ISSN 0402-1215, 1994, pp. 1 - 9
Conference Proceeding
ASME, International Gas Turbine and Aeroengine Congress and Exposition, The Hague, Netherlands; UNITED STATES; 13-16 June 1994, 06/1994
The aspirating probe originally designed by Epstein and Ng (1983) was modified by replacing the two platinum coated tungsten hot wires normally used with... 
Conference Proceeding
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