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    Efficient Trim In Helicopter Aeroelastic Analysis 

    Chandra Sekhar, D (2011-04-06)
    Helicopter aeroelastic analysis is highly complex and multidisciplinary in nature; the flexibility of main rotor blades is coupled with aerodynamics, dynamics and control systems. A key component of an aeroelastic analysis ...

    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 ...

    Piezoceramic Dynamic Hysteresis Effects On Helicopter Vibration Control Using Multiple Trailing-Edge Flaps 

    Viswamurthy, S R (2009-07-14)
    Helicopters suffer from severe vibration levels compared to fixed-wing aircraft. The main source of vibration in a helicopter is the main rotor which operates in a highly unsteady aerodynamic environment. Active vibration ...

    Helicopter Vibration Reduction Using Single Crystal And Soft Piezoceramic Shear Induced Active Blade Twist 

    Thakkar, Dipali (2011-10-14)

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    AuthorChandra Sekhar, D (1)Pawar, Prashant M (1)Thakkar, Dipali (1)Viswamurthy, S R (1)Subject
    Aeroelastic Analysis (4)
    Aeronautics (4)
    Helicopter Rotor Blades (3)Helicopter - Aeroelasticity (2)Rotors (Helicopters) (2)Actuator Dynamic Hysteresis (1)Composite Beam (1)Composite Blade (1)Composite Helicopter Rotor (1)Composite Materials (1)... View MoreDate Issued2011 (2)2007 (1)2009 (1)Has File(s)Yes (4)

    etd@IISc is a joint service of SERC & J R D Tata Memorial (JRDTML) Library || Powered by DSpace software || DuraSpace
    Contact Us | Send Feedback | Thesis Templates
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