Flight, February 1935

MORE About the "SNARK"
Some Performance Figures for Dr. N. de Bruyne's Design: Practical Details

   FOUR seats, and a range of 500 miles, is a good performance with a "Gipsy Major" when the cruising speed is 112 m.p.h. The "Snark," designed by Dr. N. de Bruyne, of Aero Research, Ltd... Cambridge, is capable of achieving these figures, and it is probable that after further tests the all-up weight will be increased. Even at its present figure the ratio of gross weight to tare weight is as high as 1.82, which means that the machine, although a comparatively small wooden cantilever monoplane, carries 82 per cent, of its gross weight - an unusually high figure for this class of machine. This has been achieved, as was explained in Flight of December 27, 1934, by the evolution of a system of stressing which takes into full account that proportion of the stress carried by the plywood skin, both of the fuselage and the wings.
   The “Snark” embodies a number of very interesting points, quite apart from its main structural features. The control column is of the jointed type, so that the top can be swung over to allow either front passenger to fly the machine. On the rear of the top of this column is another small handle which operates the brakes; a sideways motion brakes either wheel for taxiing, while pulling backwards puts on both brakes together. This last point is valuable, in that it ensures raising the elevators at the same time that the brakes are applied. This brake lever can also be locked in the fully-on position for parking, locking the elevators at the same time; and, as the ailerons are operated by an irreversible link motion, the machine is then in a suitable state to be left unattended.
   Data are as follows:-
   WEIGHTS:- Weight empty (excluding upholstery). 1,180 lb.; all-up weight, 2,200 lb.; wing-loading, 9.3 lb./sq. ft.; power loading, 16.9 lb./h.p.; weight/span, 1.24 lb./sq. ft.
   AREAS (sq. ft.):- Wing, 216.4; ailerons, 21.6; tailplane, 16.4; elevators, 10.4; rudder, 6.6; fin, 6.7.
   PERFORMANCE (estimated):- max. speed, 120 m.p.h.; cruising speed, 112 m.p.h.; landing speed, 40 m.p.h.; initial rate of climb, 600 ft./min.; ceiling, 15,500 ft.; range, 500 miles.


AN INTERESTING CONTROL SYSTEM
The Operation of the "Swing-over" Column on the "Snark"

   OF unusual interest, the control system developed for the de Bruyne ''Snark'' deserves detail description. The machine itself was described in Flight for December 27, 1934, and February 14 this year. The drawings given above are diagrammatic in that they do not show the actual details of the system, but merely indicate the method by which the results are achieved.
   Fig. 1 is a side view of the control column, showing the bottom pivot and the connections to the ailerons. Fig. 2 is a view of the column looking aft; it explains the method whereby aileron control is obtained by hinging the top part of the column only and by arranging for that part to have its neutral position at an angle; i.e., it gives a neutral position on each side, so that either person in the front seats can take control.
   Fig. 3 is a similar view looking forward and shows the secondary lever by which the wheel-brakes are applied - differentially by a sideways movement and "both on" by a straight pull backwards. Fig. 4 shows how this brake lever is locked by a catch for holding both wheel brakes "on" when parking the machine; this method has the added attraction that locking locks the elevators up.
   The remaining drawing explains the method of operating the ailerons. By altering the length of the link and the relative positions of the centres, any combination of movement can be obtained.
   Mr. de Bruyne has primarily built the “Snark” for experimental purposes, so the results he obtains will be followed with the greatest interest. It is understood that his firm, Aero Research, Ltd., is shortly to move to an aerodrome which has been acquired by the company at Duxford, within a mile or so of the Royal Air Force aerodrome of that name.