Measurement of unsteady transition on a pitching airfoil using dynamic pressure sensors
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials
Link
http://link.springer.com/content/pdf/10.1007/s12206-016-0928-5.pdf
Reference23 articles.
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3. J. Feng, X. Luo, P. Guo and G. Wu, Influence of tip clearance on pressure fluctuations in an axial flow pump, J. of Mechanical Science and Technology, 30 (4) (2016) 1603–1610.
4. C. F. Knapp and P. J. Roache, A combined visual and hotwire anemometer investigation of boundary-layer transition, AIAA J., 6 (1) (1968) 29–36.
5. J. E. Lagraff, Observations of hypersonic boundary-layer transition using hot wire anemometry, AIAA J., 10 (6) (1972) 762–769.
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