Rolls-Royce Archives
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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).
Table of tensile test results for various alloys at different temperatures.

Identifier  ExFiles\Box 36\3\  scan 096
Date  28th June 1917 guessed
  
TENSILE TESTS

No. Designation. Temperature. Maximum stress. Yield point. Elongation. Reduction in area.
(1) F1 ( 20°C tons tons
( 220°C 7.2 6.0 2.0 2.3
( 270°C 6.4 5.2 0.3 0.3
( 320°C 8.0 6.0 0.5 0.5
( 400°C 6.6 5.2 1.0 0.9
2.60 5.5 4.9

(2) F2 ( 20°C 7.2 4.4 3.3 3.3
( 220°C 6.8 4.4 2.3 2.8
( 270°C 6.4 4.8 2.9 3.0
( 320°C 5.8 4.4 3.0 3.2

(3) C ( 20°C 9.6 8.0 2.8 3.0
( 220°C 5.2 4.4 4.0 4.1
( 270°C 4.8 4.0 5.4 5.4
( 320°C 4.6 3.6 5.5 5.3

(4) M1 ( 20°C 9.2 8.0 2.0 2.5
( 220°C 4.0 2.4 0.5 0.5
( 270°C 3.2 2.4 0.5 0.5
( 320°C 3.2 2.4 1.0 1.0

(5) L ( 270°C 5.2 4.0 4.2 4.8
( 320°C 5.8 2.6 5.0 5.0

(6) H ( 20°C 9.2 7.2 5.0 4.7
( 220°C 7.4 6.0 6.5 5.8
( 270°C 6.4 4.8 6.5 5.8
( 320°C 6.6 4.8 6.5 5.8
( 400°C 2.60 10.0 9.0

(7) A ( 20°C 7.2 5.6 1.0 1.0
( 220°C 6.6 4.8 0.5 0.5
( 270°C 6.8 4.8 1.5 1.5
( 320°C 6.6 4.4 1.0 0.8

(8) M2 ( 20°C 5.2 3.2 1.0 1.0
( 220°C 5.2 2.8 2.5 3.0
( 270°C 3.0 2.0 0.5 0.5
( 320°C 3.2 2.4 6.0 5.0

There should have been 6 specimens of each alloy,
but owing to scrap, some of these are mising on the list.

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