| Download | - View final version: A note on the deflection of the engine mount in No. 4 test cell (PDF, 597 KiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003775 |
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| Author | Search for: Stephenson, D. G.1 |
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| Affiliation | - National Research Council Canada. National Aeronautical Establishment
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| Format | Text, Memorandum |
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| Physical description | 2 p. |
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| Abstract | During my recent visit to Α. V. Roe, I was asked by Mr. Knowles whether the N.A.E. had any plans for building an altitude test bed for Jet engines. He said that the matter had been considered earlier by Avro and a rough design estimate of $75,000 had been mentioned. In their proposal it had been intended to construct a simple altitude chamber in which the engine would be mounted. At the discharge end it was proposed to inject steam from the large Nobel powerhouse and thus induce an air flow through the chambers. An expansion turbine at the entrance would permit the desired depression to be obtained. |
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| Publication date | 1951-10-31 |
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| Publisher | National Research Council Canada |
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| Series | |
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| Language | English |
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| Peer reviewed | No |
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| Export citation | Export as RIS |
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| Report a correction | Report a correction (opens in a new tab) |
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| Record identifier | ef09148b-a06e-4069-b42b-2329c328fc84 |
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| Record created | 2025-10-02 |
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| Record modified | 2025-12-01 |
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