Aeroelastic Optimization of High-Speed Tiltrotor Wings with Wing Extensions and Winglets-Reference-Cited by-同舟云学术

Aeroelastic Optimization of High-Speed Tiltrotor Wings with Wing Extensions and Winglets

Published:2017-09 Issue:5 Volume:54 Page:1718-1727
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Kambampati Sandilya¹,Smith Edward C.¹

Affiliation:

1. The Pennsylvania State University, University Park, Pennsylvania 16802

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034195

Reference17 articles.

1. Parametric Studies for Tiltrotor Aeroelastic Stability in Highspeed Flight

2. Aeroelastic stability of wing/pylon/rotor coupled system for tiltrotor aircraft in forward flight

3. Results of an Aeroelastic Tailoring Study for a Composite Tiltrotor Wing

4. AcreeC. Jr.PeyranR.JohnsonW. “Rotor Design Options for Improving XV-15 Whirl-Flutter Stability Margins,” NASA TP-2004-212262, 2004.

5. WhitcombR. T. “A Design Approach and Selected Wind Tunnel Results at High Subsonic Speeds for Wing-Tip Mounted Winglets,” NASA TN D-8260, July 1976.

Cited by 12 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 numerical research on the hydrodynamic performance of marine propellers with bionic coupled blade sections;Ships and Offshore Structures;2024-05-23

2. Preliminary Design and Optimization of Primary Structures for a Tilt-Duct UAV;Aerospace;2024-04-08

3. Exploration of the Effects of Rotor Blade Twist on Whirl-Flutter Stability Boundaries;Journal of Aircraft;2023-09-18

4. Optimal Tiltrotor Blade Twist to Extend Whirl-Flutter Stability Boundaries;AIAA SCITECH 2023 Forum;2023-01-19

5. Whirl Flutter Suppression of Tiltrotor Aircraft Using Actively Controlled Aileron;Aerospace;2022-12-04