COMBAT AND COMPETITION.pdf - Lakes Gliding Club
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