A wind tunnel test model structure with a high slenderness ratio belongs to the field of wind tunnel test vehicle
design technology. It solves the problems of large
vibration amplitude and low
data accuracy in existing technologies during testing. Key technical points: The
rectifier cap, front cylinder, and front port
flange are sequentially bonded together, with the front port
flange connected to the front end of the central steel shell; the rear port
flange, rear end cylinder, and rear end plate are sequentially bonded together, with the rear port flange connected to the rear end of the central steel shell; a balance sleeve is fitted onto the balance, the central steel shell is fitted onto the balance sleeve, the balance front cone tension plate is connected to the central steel shell, the front end of the balance is connected to the balance front cone tension plate, and the rear end of the balance is connected to the
tail end of the balance sleeve. This invention significantly reduces the
vibration amplitude of the model structure during testing, avoids damage to the model and equipment caused by
resonance, and improves the safety and stability of the entire wind tunnel
high angle-of-
attack test process; it effectively suppresses the interference of model vibration on measurement results, ensuring accurate and reliable
test data acquisition.