Transonic moist air flow around a circular arc blade with bump
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-009-0325-9.pdf
Reference12 articles.
1. Lee, B.H.K.: Self-Sustained Shock Oscillations on Airfoils at Transonic Speeds, Progress in Aerospace Sciences, vol. 37, pp.147–196, (2001).
2. Ranhunathan, S., Gillan, M.A., Cooper, R.K., Mitchell, R.D., Cole, J.S.: Shock Oscillations on biconvex aerofoils, Aerospace Science and Technology, vol. 3, pp. 1–9, (1999).
3. Urbassik, R.M., Wolff, J.M., Polanka, M.D.: Unsteady Aerodynamics and Interactions between a High-Pressure Turbine Vane and Rotor, Transaction of the ASME, Journal of Turbomachinery, vol. 128, pp. 35–42, (2006).
4. Tulita, C., Rangunathan, S., Benard, E.: Control of Transonic Periodic Flow on NACA0012 Aerofoil by Contour Bump, Proc. IUTAM Symposium Transsonicum IV, pp. 291–296, Göttingen, Germany, (September 2002).
5. Stanewsky, E.: Aerodynamic Benefits of Adaptive Wing Technology, Aerospace Science and Technology, vol. 4, pp. 147–156, (2000).
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