A novel data reduction technique for single slanted hot-wire measurements used to study incompressible compressor tip leakage flows

Author:

Berdanier Reid A.ORCID,Key Nicole L.

Funder

National Aeronautics and Space Administration

National Science Foundation

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference23 articles.

1. Berdanier RA (2015) An experimental characterization of tip leakage flows and corresponding effects on multistage compressor performance. PhD dissertation, School of Mechanical Engineering, Purdue University, West Lafayette

2. Berdanier RA, Key NL (2016) The effects of tip leakage flow on the performance of multistage compressors used in small core engine applications. ASME J Eng Gas Turbine Power 138:052605-1–052605-10

3. Blidi S, Miton H (1995) Use of the hot wire anemometry for velocity and temperature measurements in a turbomachine. J Phys III 5:1513–1535

4. Collis DC, Williams MJ (1959) Two dimensional convection from heated wires at low Reynolds numbers. J Fluid Mech 16:357–384

5. Cukurel B, Acarer S, Arts T (2012) A novel perspective to high-speed cross-hot-wire calibration methodology. Exp Fluids 53:1073–1085

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