| Download | - View final version: Shock strut deflections and the corresponding angle of thrust-line to horizontal of two-ski landing gear for aircraft (PDF, 1.3 MiB)
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| DOI | Resolve DOI: https://doi.org/10.4224/40003452 |
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| Author | Search for: Mandl, P.1; Search for: National Research Council of Canada. Division of Mechanical Engineering. Aerodynamics Section |
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| Affiliation | - National Research Council of Canada
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| Format | Text, Technical Report |
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| Physical description | 19 p. |
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| Abstract | It was desired to analyse the behaviour of the front and rear shock absorbers of a two-ski landing gear for an aircraft passing from level ground on to a slope of ± 10 at speeds of 20, 40 and 60 m.p.h. |
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| Publication date | 1946-03-22 |
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| Publisher | National Research Council of 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 | 0fe54c43-97ee-46dc-a92a-7754e6b8330a |
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| Record created | 2025-01-13 |
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| Record modified | 2025-01-13 |
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