Analysis of structures with rotating, flexible substructures appliedto rotorcraft aeroelasticity
- 1 February 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (2), 192-200
- https://doi.org/10.2514/3.10081
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Structured data in structural analysis softwareComputers & Structures, 1987
- Application of GRASP to nonlinear analysis of a cantilever beamPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Analysis of structures with rotating, flexible substructuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Introduction to GRASP—General Rotorcraft Aeromechanical Stability Program—A Modern Approach to Rotorcraft ModelingJournal of the American Helicopter Society, 1987
- Assessment of aerodynamic and dynamic models in a comprehensive analysis for rotorcraftComputers & Mathematics with Applications, 1986
- Spacecraft DynamicsJournal of Applied Mechanics, 1983
- Orthogonal polynomials as variable-order finite element shape functionsAIAA Journal, 1983
- An Aeromechanical Stability Analysis for Bearingless Rotor HelicoptersJournal of the American Helicopter Society, 1979
- Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in HoverJournal of the American Helicopter Society, 1972
- A linearization tool for use with matrix formalisms of rotational dynamicsArchive of Applied Mechanics, 1969