By L. Johansson
Plane layout three (2000) 249 - 259
In this paper the adventure of the writer in operating a flight dynamics direction with MATLAB computer
assignments as a wide a part of the direction and the only technique of review is mentioned.
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Additional info for A flight dynamics course based on MATLAB computer assignments
Single engine performance was, however, inferior to earlier experience; the maximum weight for the maintenance of height was found to be 26,500 lb. The apparent deterioration was attributed to high abient temperatures reducing density and also causing drag from the open radiator flaps. The final trial on Z9467 with Halifax-type Rotol propellors produced a 17% increase in rate of climb at the expense of cruising speed. Aerial mines were released cleanly from Z6649 early in 1942-the installation AD Type H being common to several types.
A month later, Z6640 was loaded to 32,000 Ib at take-off; at this weight the single engine rate of descent was 320 ft/min at 76 4,000 ft; standard take-off run was 665 yd, and 50 ft reached after 1,000 yd. 5°e. Two short trials in the spring of 1942 demon-strated that the radiator provided sufficient cooling for the tropics (BD231) and that flame damping (NI375) met current requirements. roles of glider tug and anti-submarine was limited, starting with T4223 for the latter duty for three days in ovember 1939.
The work o[ the Section included advice to trials officers on the best and most e[ficientmethods for conducting tests, trials, assistance in the resolution of problems and developmcnt of instrumentation. In 1943, Mr G. Standcn evolved a method of measuring the loads on the ammunition, links, feeds and assisters when gun firing. 5 ton psi on the wing spar. 5 mm) to 75 mm came under the scrutiny of the Gunncry Section between 1939 and 1945 in nearly 100 types of aircraft. l; dcscribed here are the testing and development of new and modified weapons in both fixcd and free mountings, and in turrets.