British Full-Scale Wind-Tunnel & Turbulence (i.e. why they thought the Beaufighter could do 370 mph)

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The performance of the Vulture version wasn't too far off - 428mph vs ~400mph for the actual aircraft. Though I am not sure about the speed being achieved at 190,000ft!

There was a change in the radiator design of the Tornado early in the testing program. Might that have something to do with performance overestimation too? Was the initial Typhoon design also with a ventral radiator?

Calum, do you have the estimated engine power for those performance estimates?
 
I found this interesting paper, which had the answer I was looking for:

The second question is why was not the tunnel made bigger and why was the speed limited to 115 m.p.h. A tunnel to test even the smaller of the best service aircraft under maximum speed conditions would require twice the cross section and at least three times the speed, so that instead of the present 2,000 h.p. for the fan, 100,000 h.p. would be required. Increase of size leads to reduction in sensitivity of balances and increased time on rigging and repair. The tunnel built represents a very convenient compromise for the type of work for which it is intended.​

COOLING PROBLEMS, WITH PARTICULAR REFERENCE TO THE WORK OF THE 24ft. R.A.E. TUNNEL
BY G. P. DOUGLAS, M.C., D.Sc., A.F.R.Ae.S.
Royal Aeronautical Society Proceedings Lecture November 18th, 1935.
 

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This is why the German built wind tunnels in the Austrian Alps next to dams. IIRC, at least one was a direct, physical drive like a watermill. No generators.
 
One of the best aerobatic demo ever senn was by one Bevo (Beverly) Howard in a 1949 V-tail Bonanza. Beverly used to be a semi-popular boy's name.
 

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