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Bristol Aeroplane Company Limited. Stress Department.Engine stress investigation:...
Catalogue reference: PA1716/5/11/2/349
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This record is a file about the Bristol Aeroplane Company Limited. Stress Department.Engine stress investigation:... dating from 29 June 1954.
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Full description and record details
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Reference (The unique identifier to the record described, used to order and refer to it)
- PA1716/5/11/2/349
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Title (The name of the record)
- Bristol Aeroplane Company Limited. Stress Department.Engine stress investigation: Olympus 6 LP compressor rotor blades.
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Date (When the record was created)
- 29 June 1954
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Description (What the record is about)
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Ref: 4366/2.By RSL Pritchard. Stresses in Olympus 6 LP compressor rotor blades under various aerobatic conditions. Previous calculations referred to 4316/2, 4366SR/2, 8 August 1952. Contents Page 1 summary; Evaluation of factors for the engine conditions pages 2 & 3; data given Page 3; Calculation of correction factors pages 4-8
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Held by (Who holds the record)
- Coventry Archives & Research Centre
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Language (The language of the record)
- English
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Physical description (The amount and form of the record)
- 1 Item
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Record URL
- https://beta.nationalarchives.gov.uk/catalogue/id/d77742e1-1c6c-4151-9e3e-c0cd482902eb/
Series information
PA1716/5/11/2
Bristol Gas Turbines: Olympus stress reports & calculations for all models
See the series level description for more information about this record.
Catalogue hierarchy
This record is held at Coventry Archives & Research Centre
Within the fonds: PA1716
Rolls-Royce Heritage Trust, Coventry Branch - Records of Armstrong Siddeley, Bristol...
Within the sub-fonds: PA1716/5
Armstrong Siddeley/Bristol Siddeley & Rolls-Royce Gas Turbines
Within the sub-sub-fonds: PA1716/5/11
Olympus Engine
Within the series: PA1716/5/11/2
Bristol Gas Turbines: Olympus stress reports & calculations for all models
You are currently looking at the file: PA1716/5/11/2/349
Bristol Aeroplane Company Limited. Stress Department.Engine stress investigation: Olympus 6 LP compressor rotor blades.