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COMBAT AND COMPETITION.pdf - Lakes Gliding Club

COMBAT AND COMPETITION.pdf - Lakes Gliding Club

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CHAPTER ELEVEN A TESTING TIME<br />

to its designers, who were now operating from Twinwood Farm, and<br />

Horace put them under great pressure. He was most unhappy about the<br />

rumours which had originated from Camphill and wanted confirmation<br />

of the performance as soon as possible.<br />

Stable conditions were essential and it took almost eight months to<br />

complete the tests - just five days being suitable during the whole of<br />

that time. One flight was typical of the problems which they faced.<br />

Starting even earlier than usual - out of bed at 3 am - to be<br />

confronted with an unbroken layer of stratus 200 feet thick, base 800<br />

feet above the ground. The plan - for Roger Austin to find the airfield<br />

after the tow and mark it by circling in the tug, while Harry made his<br />

partial glides - misfired completely. After release they never saw each<br />

other again. Harry broke cloud some miles away and had to land out.<br />

A new technique was used to record the raw data. On each partial<br />

glide, the pilot reported his height by radio at 50 foot intervals. Ralph<br />

Maltby and his two assistants, one armed with a stopwatch, plotted time<br />

against height straight onto a chart. The effect of any disturbance was<br />

instantly apparent and the pilot could be instructed to continue his run<br />

over a further thousand feet.<br />

The maximum gliding angle of 1 in 33.5 compared with the original<br />

design at I in 26.5, was a total vindication of their efforts. But the<br />

minimum sink was slightly greater than expected and it occurred at 44<br />

knots.<br />

When I joined Harry's test group, after the 1955 Nationals, we<br />

carried out pilot rake and china clay/paraffin tests on an inboard<br />

section of mainplane. But they showed no evidence of premature<br />

laminar separation.<br />

Before the aircraft left Twinwood, Ralph managed to organise wind<br />

tunnel tests on one wing, using the aileron as a flap. Intended to<br />

confirm their extrapolation of relevant NACA 4 information, to glider<br />

Reynolds numbers, this may well have been the origin of the 'no<br />

substitute for span' philosphy of the later developments.<br />

The 402 arrived at Twinwood two weekends before Easter. Barely<br />

time to sort out any problems and obtain a temporary C of A for an<br />

entry in the first contest of the year, the Long Mynd Easter Rally. If<br />

it proved good enough there was just a possibility that it might be<br />

flown by the British team in the World Championships now only<br />

months away.<br />

We got there, but only just. To avoid altering the aileron hinge<br />

line, the tip chord on the extended wing had become almost 80%<br />

175

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