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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).
Moment of Inertia tests performed on a valve rocker assembly.

Identifier  ExFiles\Box 88\4\  scan0132
Date  18th February 1935
  
VALVE ROCKERS - M.{Mr Moon / Mr Moore} I. TESTS.
Eº 41590 ROCKER - COMPLETE WITH BUSHES, PLUGS, & ADJUSTING SCREW.
¢ OF ADJUSTING SCREW AT RT. ∠s TO ¢ OF PENDULUM.

TEST 1. ROCKER OUTSIDE PENDULUM.
PERIODIC TIME.
PENDULUM + ROCKER E₁₁ = .8475 SECS.
ONLY E₁ = .756 "

WEIGHTS
PENDULUM W₁ = 200 GRAMMES
ROCKER W₁₁₁ = 126 "
PENDULUM + ROCKER W₁₁ = 326 "

CENTRE OF GRAVITY
WITH ROCKER x̄₁₁ = 5.24"
WITHOUT " x̄₁ = 3.788"

M.I. WITH ROCKER - ABOUT AXIS OF SUSPENSION.
I_s = (.8475² x 326 x 5.24) / (4π² x 28.35 x 16 x 12) = .005709

M.I. WITHOUT ROCKER - ABOUT AXIS OF SUSPENSION
I_s = (.756² x 200 x 3.788) / (4π² x 28.35 x 16 x 12) = .002014

TEST 2. ROCKER INSIDE PENDULUM.
PERIODIC TIME. t₁₁ = .755 SECS t₁ = .756 SECS
WEIGHT W₁ = 200 GRAMMES, W₁₁₁ = 126 GRAMMES, W₁₁ = 326 GRAMMES.
C.O.G. x̄₁₁ = 4.27 x̄₁ = 3.788"

M.I. WITH ROCKER - ABOUT AXIS OF SUSPENSION.
I_s = (.755² x 326 x 4.27) / (4π² x 28.35 x 16 x 12) = .00369.

M.I. WITHOUT ROCKER - ABOUT AXIS OF SUSPENSION.
I_s = .002014.

HB{C. E. Harcombe}
  
  


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