Showing items related by title, author, creator and subject.

• Prediction of Physical Behavior of Rotating Blades under Tip-Rub Impact using Numerical Modeling 

  Subramanya, S (2018-02-09)

  Rotating blades, which are the most critical components of any turbo-machinery, need to be designed to withstand forced vibrations due to accidental tip rub impact against inner surface of casing. These vibrations are ...

• Aeroelastic Analysis And Optimization Of Composite Helicopter Rotor With Uncertain Material Properties 

  Murugan, M Senthil (2011-04-06)

  Incorporating uncertainties in the aeroelastic analysis increases the confidence levels of computational predictions and reduces the need for validation with experimental or flight test data. Helicopter rotor blades, which ...

• Structural Health Monitoring Of Composite Helicopter Rotor Blades 

  Pawar, Prashant M (Indian Institute of Science, 2007-04-18)

  Helicopter rotor system operates in a highly dynamic and unsteady aerodynamic environment leading to severe vibratory loads on the rotor system. Repeated exposure to these severe loading conditions can induce damage in the ...