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Optimal Micro-Scale Secondary Flow Control for the Management of High Cycle Fatigue and Distortion in Compact Inlet DiffusersThe purpose of this study on micro-scale secondary flow control (MSFC) is to study the aerodynamic behavior of micro-vane effectors through their factor (i.e., the design variable) interactions and to demonstrate how these statistical interactions, when brought together in an optimal manner, determine design robustness. The term micro-scale indicates the vane effectors are small in comparison to the local boundary layer height. Robustness in this situation means that it is possible to design fixed MSFC robust installation (i.e.. open loop) which operates well over the range of mission variables and is only marginally different from adaptive (i.e., closed loop) installation design, which would require a control system. The inherent robustness of MSFC micro-vane effector installation designs comes about because of their natural aerodynamic characteristics and the manner in which these characteristics are brought together in an optimal manner through a structured Response Surface Methodology design process.
Document ID
20020061367
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Anderson, Bernhard H.
(NASA Glenn Research Center Cleveland, OH United States)
Keller, Dennis J.
(RealWorld Quality Systems, Inc. Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2002
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2002-211686
E-13415
NAS 1.15:211686
Report Number: NASA/TM-2002-211686
Report Number: E-13415
Report Number: NAS 1.15:211686
Funding Number(s)
PROJECT: RTOP 708-53-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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