Tip clearance

From Wikipedia, the free encyclopedia
The inlet of an EJ200, showing rotor and stator blades. The narrow clearance between the rotor (first set of blades) and the casing is visible.

Tip clearance is the distance between the tip of a rotating airfoil and a stationary part.

References

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  1. ^ Page Module:Citation/CS1/styles.css has no content.Boyce, Meherwan P. (2002). Gas turbine engineering handbook. Gulf Professional Publishing. p. 365. ISBN 0-88415-732-6. Retrieved 2009-03-16. gas turbine tip clearance.
  2. ^ Page Module:Citation/CS1/styles.css has no content.Breslin, John P.; Poul Andersen (1996). Hydrodynamics of Ship Propellers. Cambridge University Press. p. 424. ISBN 0-521-57470-6. Retrieved 2009-03-16.
  3. ^ Page Module:Citation/CS1/styles.css has no content.Burton, Tony; David Sharpe; Nick Jenkins; Ervin Bossanyi (2001). Wind Energy Handbook. John Wiley and Sons. p. 464. ISBN 0-471-48997-2. Retrieved 2009-03-16.