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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).
Comparison of gauge and weight ratios for steel versus light alloys (Aluminium and Magnesium) in various automotive components.

Identifier  ExFiles\Box 154a\1\  scan0275
Date  7th March 1940
  
Rm{William Robotham - Chief Engineer}/FJH.{Fred J. Hardy - Chief Dev. Engineer}24/MR.7.3.40.

STEEL AND LIGHT ALLOY COMPARISONS
BASED ON Rm.{William Robotham - Chief Engineer}609.

(1) Frames of constant dimensions but varying gauge. Deflection to be constant.

Comparison based on Tensile stress and constant elongation.

Ratio of gauges Al/Steel = 3.00 : 1
" " " Mg/Steel = 5.00 : 1
" " weights Al/Steel = 1.07 : 1
" " " Mg/Steel = 1.05 : 1

(2) Axle Tube of constant mean dia. and strength.

Comparison based on Tensile stress and constant strength.

Ratio of thickness Al/Steel = 1.50 : 1
" " " Mg/Steel = 2.00 : 1
" " weights Al/Steel = 0.536: 1
" " " Mg/Steel = 0.461: 1

(3) Body panel of constant shape but varying gauge.

Comparison based on beam of constant width and:-

(a) Constant Deflection.

Ratio of gauges Al/Steel = 1.44 : 1
" " " Mg/Steel = 1.71 : 1
" " weights Al/Steel = 0.52 : 1
" " " Mg/Steel = 0.40 : 1

(b) Constant Strength.

Ratio of guages Al/Steel = 1.22 : 1
" " " Mg/Steel = 1.41 : 1
" " weights Al/Steel = 0.44 : 1
" " " Mg/Steel = 0.33 : 1

Rm{William Robotham - Chief Engineer}/FJH.{Fred J. Hardy - Chief Dev. Engineer}
  
  


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