by Ganguli R.
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NPR 16940
NPR 13552
ISBN 13 | 9789811060977 |
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Edition | 1st |
Year | 2018 |
Publisher/Company | Springer |
Language | English |
The book is readers-friendly which addresses computational methods for solving the problem of vibration, response, loads and stability of a helicopter rotor blade modeled as a rotating beam with flap or out-of-plane bending. The contents of the book is useful to researchers in aerodynamics and professionals working in the aerospace industry. It focused on explaining and briefing in the implementation of the finite element method in the space and time domain for the free vibration, aero elastic response and stability problems.
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