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From the Rolls-Royce experimental archive: a quarter of a million communications from Rolls-Royce, 1906 to 1960's. Documents from the Sir Henry Royce Memorial Foundation (SHRMF).
Performance data comparison for three different radiator core configurations under specific temperature and waterflow conditions.

Identifier  ExFiles\Box 149a\2\  scan0020
Date  6th February 1932
  
6-2-32

ROLLS ROYCE CORE

180° TOP TANK - 100° AIR - 35 G.P.M. WATERFLOW

Note: The 1/4 T.H. x 3-1/4 and 1/4 T.H. x 4 Zig Zag cores
were estimated to Rolls Royce R.M. from tests made
on 17 x 17 test sections.
(All Temperatures are in degrees F.{Mr Friese})

#7266-1
.25 x .45 x 3-1/4 1/4 T.H. x 3-1/4 1/4 T.H. x 4
x .044 - Reg.Prod. A.C. Zig Zag A.C. Zig Zag
A.C. V-Vee-5 bump
NEW MATRIX

Frontal Area 456 456 456
Diss. Effective Area 430 430 430

C.F.M. @ 30 3055 4400 3830
@ 40 4100 5930 5270
@ 60 6435 9200 8350
@ 80 8340 12390 11200
@ 100 10800 15480 13920

Air Velocity @ 30 10.65 16.77 14.61
@ 40 15.65 22.60 20.15
@ 60 24.55 35.10 31.85
@ 80 31.80 47.20 42.70
@ 100 41.10 58.80 53.10

Air Rise @ 30 46.4 27.3 32.0
@ 40 43.8 23.9 27.9
@ 60 38.9 20.3 23.8
@ 80 36.1 18.3 22.1
@ 100 32.7 17.2 20.6

Water Drop @ 30 8.2 6.95 7.09
@ 40 10.4 8.2 8.5
@ 60 13.75 10.8 11.5
@ 80 17.4 13.1 14.4
@ 100 20.4 15.5 16.6

B.T.U./Min. @ 30 2325 1975 2015
@ 40 2950 2330 2420
@ 60 3900 3070 3270
@ 80 4950 3720 4080
@ 100 5800 4390 4715


W. O.{Mr Oldham} Emmons
  
  


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