Design and Development
The CL-41 design was the product of the Canadair Preliminary Design department. The design incorporated a turbojet-powered, low-wing monoplane with a tricycle undercarriage and a T-type tail assembly. The flying controls are manual with spring tabs. The cabin, fitted with a rear-hinged canopy for both crew members, can be pressurized to a differential of 3 psi (20 kPa), the equivalent of about 2,000 m of altitude. It was designed to be a side-by-side trainer for providing elementary jet flight training and other training to an advanced level. The prototype first flew on 13 January 1960.
One critical area of design was the positioning of the vertical stabilizer (fin). The CL-41 was intended to demonstrate spin recovery. If the fin is too far forward, spin can not be initiated, but if it is too far aft, recovery becomes impossible. Model tests were done to find the optimum position. The original Tutor wind-tunnel model had a cruciform tail, which was revised to the T-tail design by removing the portion above the horizontal stabilizer.
Read more about this topic: Canadair CT-114 Tutor
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