Research progress on analysis and test methods of aircraft panel flutter
Aircraft panel flutter is a typical aeroelastic stability problem that occurs during supersonic flight,and is characterized by aerodynamic unilateral effects and significant structural and aerodynamic nonlinearity. The current research status of panel flutter issues both domestically and abroad is r...
Saved in:
| Main Authors: | HE Chuanyang, WANG Binwen, SONG Qiaozhi, LI Xiaodong, CHEN Haoyu |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2024-12-01
|
| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2024085 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
The modern method of creating dynamically scaled models to study aircraft flutter characteristics
by: A.V. Dolgopolov, et al.
Published: (2020-12-01) -
Flutter Analysis Based on the New Numerical Model IAR-99 HAWK Empty Equipped Configuration Aircraft
by: Tudor VLADIMIRESCU, et al.
Published: (2024-12-01) -
Three-Dimensional Flutter Numerical Simulation of Wings in Heavy Gas and Transonic Flutter Similarity Law Correction Method
by: Zhe Hu, et al.
Published: (2024-11-01) -
Flutter Prediction Method for Long Blade of Steam Turbine
by: Changchun LIU, et al.
Published: (2021-08-01) -
Passive Aeroelastic Control of a Near-Ground Airfoil with a Nonlinear Vibration Absorber
by: Kailash Dhital, et al.
Published: (2024-12-01)