Design of a distributed testing system for high-dynamic vector thrust of aero-engines based on piezoelectric force-sensitive units
Fields of Study & Subjects
Aeroelasticity and Vibration Control
Hydraulic and Pneumatic Systems
Model Reduction and Neural Networks
Publication details
- Journal / source
- Measurement
- Publisher
- Elsevier BV
- Volume
- 266
- Pages
- 120436–120436
- Publication date
- 15 January 2026
- Language
- EN