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Aviation History
1928
1928 - 0990.PDF
14 OCTOBER 18, 1928 efficient aerodynamic design, resulting in a very small power requirement, and partly by clever construction which gives a most unusual ratio of weight carried to tare or empty weight. On the aerodynamic side it is seen that, to begin with, Herr Messerschmitt has chosen a fairly large span (15-6 m.) in order to keep down induced drag. As the span is 51 -2 ft. * span2 and the total loaded weight is 2,640 lb.,the ratio - . ,-• is ° .weight nearly 1, a very high figure for a commercial machine. This means that at 80 m.p.h., for instance, the cruising speed of [" FLIGHT" Sketch Sketch showing tail skid, central elevator crank andhandling rail on the B.F.W. M.18. the machine, the ratio of lift to induced drag is in the neigh- bourhood of 50. At 60 m.p.h., or somewhere in the region of the take-off speed, this ratio will still be as high as 30 or so, thus helping materially in enabling the machine to take off with a high load per horse-power. Great care in streamlining the nose of the machine, by cowling the engine, etc., has probably resulted in another reduction of drag, while the undercarriage has been kept of such an elementary form that its drag is probably also quite low, the axles springing straight out through slots in the sides of the fuselage, as shown in one of our sketches. The fuselage itself, although of the flat-sided variety, appears of reasonably- good form, and altogether the minimum drag of the M.I8 is probably extremely low. It is a little more difficult to discover how Herr Messer- schmitt has managed to keep his structure weight down to a figure which will permit the load carried by the machine to be equal to the tare weight. The fuselage is built of former, and stringers of " open " sections to facilitate inspection of rivets, &c, and covered with flat Duralumin sheet. The monoplane wing shows the same type of single spar construc- tion as the large M.20, the wing covering being Duralumin sheet over the front portion, and fabric near the trailing edge. The little cabin is quite comfortable, although naturally somewhat small, and the pilot's cockpit is well protected, while at the same time the view forward is quite good. [" Fl IGHT '* Skttl'h Details of the mounting of the wheel on the Bleriot III. The wing bracing strut is attached to the wheel centre,the wheels being internally sprung. Although designed primarily for passenger carrying, the M.18 can be used for a variety of other purposes. For instance two of the seats can be removed and the machine used for photographic work, a detachable plate in the floor making it possible to mount a camera there. The type M.18 has for some years been in service on the lines of the North Bavarian Flying Company of Furth, and is reported to have proved very satisfactory, being reliable and very economical in operation. The B.F.W. M.18 has an overall length of 8 m. (26-3 ft.), a wing span of 15-6 m. (51-2 ft.), and a wing area of 24-5 sq. m. (264 sq. ft.). The tare weight is 600 kg. (1,320 lb.) and the permissible load 600 kg., giving a total loaded weight of 1,200 kg. (2,640 lb.). The engine is a Siemens radial, type S.H.I2, rated at 100 h.p. at normal revolutions. The power m S m m m m The Palmer Stand at Berlin Show. In the centre is seen the demonstration model of the new aircraft wheel brake. m m 920
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