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Modeling and analysis of tilt-rotor aeromechanical phenomena

  • Published:1998-06 Issue:12 Volume:27 Page:17-43
  • ISSN:0895-7177
  • Container-title:Mathematical and Computer Modelling
  • language:en
  • Short-container-title:Mathematical and Computer Modelling

Author:

Barkai S.M.,Rand O.,Peyran R.J.,Carlson R.M.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modelling and Simulation

Reference31 articles.

1. Historical development of aircraft flutter;Garrick;Journal of Aircraft,1981

2. Prop-rotor stability at high advance ratio;Hall;Journal of the American Helicopter Society,1966

3. Investigation of tilt rotor VTOL aircraft rotor-pylon stability;Edenborough;Journal of Aircraft,1968

4. Dynamic structural aeroelastic stability testing of the XV-15 tilt rotor research aircraft;Schroers;NASA TM-84293,1982

5. In-flight structural dynamic characteristics of the XV-15 tilt-rotor research aircraft;Bilger;AIAA Paper 81-0612,1981

Cited by 24 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A Novel Aerodynamic Modeling Method Based on Data for Tiltrotor evtol;Applied Sciences;2024-05-10

2. Evaluation of dynamic loads and performance indexes in tiltrotors using a mid-fidelity aeroservoelastic tool;Aerospace Science and Technology;2024-03

3. Evaluation of Steady and Periodic Trim Loads in Tiltrotors using Multibody - Mid-fidelity Aerodynamic Simulations;AIAA SCITECH 2024 Forum;2024-01-04

4. Research on Rotor Speed Optimization Strategy of TiltRotor Aircraft based on IPSO-SQP Algorithm;2023 International Conference on Computer Science and Automation Technology (CSAT);2023-10-06

5. Optimal Transition Trajectory Search for Tilt-Rotor Aircraft Based on Ant Colony Algorithm;2023 2nd International Conference on Artificial Intelligence and Computer Information Technology (AICIT);2023-09-15
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