High Temperature Evaluation of an Active Clearance Control System Concept-Reference-Cited by-同舟云学术

High Temperature Evaluation of an Active Clearance Control System Concept

Published:2006-07-09 Issue: Volume: Page:
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Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Taylor Shawn,Steinetz Bruce,Oswald Jay

Publisher

American Institute of Aeronautics and Astronautics

Reference8 articles.

1. 1Lattime,S.B.,Steinetz,B.M.,Robbie,M.“TestRigforEvaluatingActiveTurbineBladeTipClearanceControlConcepts,” NASA/TM-2003-212533, also AIAA-2003-4700, presented at theAIAA/ASME/SAE/ASEE conference, July, 2003, Huntsville, AL. Journal of Propulsion and Power, vol. 21 no.3, May-June 2005.

2. 2Steinetz, B.M., Lattime, S.B., Taylor, S., DeCastro, J.A., Oswald, J., Melcher, K.A. “Preliminary Evaluation of an Active Clearance Control System Concept,” NASA/TM-2005-213856, also AIAA-2005-3989. Presented at the2005 AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Tucson, AZ.

3. 3Steinetz, B.M., Taylor, S., Oswald, J., and DeCastro, J.A. “Seal Investigations of an Active Clearance Control System Concept,” NASA/TM-2006-214114, also 120-ISROMAC-11. Presented at the11thInternational Symposium of Rotating Machinery, Honolulu, HI.

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