Active aeroelastic tailoring with adaptive continuous control surfaces-Reference-Cited by-同舟云学术

Active aeroelastic tailoring with adaptive continuous control surfaces

Published:2000-04-03 Issue: Volume: Page:
ISSN:
Container-title:41st Structures, Structural Dynamics, and Materials Conference and Exhibit
language:
Short-container-title:

Author:

Weisshaar Terrence¹,Duke David¹,Dobbins Abigail¹

Affiliation:

1. Purdue Univ., West Lafayette, IN

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-1619

Reference18 articles.

1. Aeroelastic tailoring - Theory, practice, and promise

2. Mission Adaptive Wing System for Tactical Aircraft

3. M. Waddoups, C. Smith, and R. McMickle, "Composite Wing for Transonic Improvement; Vol.I- Composite Wing Aeroelastic Response Study,"Air Force Flight Dynamics Laboratory, Technical Report AFFDL-TR-71-24, Wright Patterson AFB, Ohio, 1972.

4. E. Levinsky and et. al. "Wind Tunnel Test of an Improved Computer-Controlled Variable-Geometry Wing (Self-Optimizing Flexible Technology Wing Program)," Arnold Engineering Development Center, Technical Report AEDC-TR-80-42,1981.

5. Adaptive aeroelastic composite wings—Control and optimization issues

Cited by 4 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. Transient response study on rolling effectiveness of multiple control surfaces;Journal of Fluids and Structures;2004-06

2. Sensitivity of Optimized Structures to Constraints and Performance Requirements for the SensorCraft ISR Platform;44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2003-04-07

3. Experimental and Theoretical Study on Rolling Effectiveness of Multiple Control Surfaces;AIAA Journal;2003-02

4. Integrated wing design with adaptive control surfaces;19th AIAA Applied Aerodynamics Conference;2001-06-11