Helicopter trim analysis by shooting and finite element methods withoptimally damped Newton iterations
- 1 February 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (2) , 225-234
- https://doi.org/10.2514/3.11659
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Numerical Solution of Boundary Value Problems for Ordinary Differential EquationsPublished by Society for Industrial & Applied Mathematics (SIAM) ,1995
- Shape functions for mixed p-version finite elements in the time domainJournal of Sound and Vibration, 1991
- Weak Hamiltonian finite element method for optimal control problemsJournal of Guidance, Control, and Dynamics, 1991
- A study of symbolic processing and computational aspects in helicopter dynamicsJournal of Sound and Vibration, 1990
- Nonlinear response and stability analysis of beams using finite elements in timeAIAA Journal, 1988
- Helicopter rotor dynamics by finite element time approximationComputers & Mathematics with Applications, 1986