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A new force-measuring balance for large-scale model in hypersonic wind tunnel
Qinchao Wang1, Shichao Li1, Hongli Gao1
1School of Mechanical Engineering, SouthWest Jiaotong University, Chengdu 610031, People's Republic of China.
A novel large-scale strain balance design overcomes coupling issues in hypersonic vehicle testing. This innovation enables accurate aerodynamic load measurements for heavy-duty models in pulse wind tunnels.
Area of Science:
- Aerospace Engineering
- Fluid Dynamics
- Experimental Physics
Background:
- Hypersonic vehicle research faces challenges with integrated body-propulsion coupling.
- Scaled-down models inadequately represent physical laws for hypersonic aerodynamics.
- Testing large-scale aircraft models is crucial but difficult.
Purpose of the Study:
- To present a design for a large-scale, heavy-load, three-component strain balance.
- To address the coupling effects and stiffness issues in hypersonic aerodynamic testing.
- To enable accurate aerodynamic load measurements for large-scale hypersonic models.
Main Methods:
- Innovative "herringbone" force measuring element design for enhanced sensitivity and reduced channel coupling.
- Integration of a support plate to improve main channel sensitivity.
- Addition of convex plates at the model-balance contact surface to enhance stiffness.
Main Results:
- The developed strain balance effectively minimizes channel coupling.
- Enhanced stiffness accommodates large-scale models in wind tunnel tests.
- Static calibration and wind tunnel tests confirm the balance meets aerodynamic load test requirements.
Conclusions:
- The designed large-scale strain balance successfully overcomes key challenges in hypersonic aerodynamic testing.
- The innovative design ensures accurate measurements for heavy-duty hypersonic vehicle models.
- This facilitates more reliable research in hypersonic flight dynamics.
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