Zobrazeno 1 - 10
of 682
pro vyhledávání: '"Transport aircraft"'
Publikováno v:
International Journal of Structural Integrity, 2024, Vol. 15, Issue 6, pp. 1169-1199.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/IJSI-07-2024-0108
Publikováno v:
Xibei Gongye Daxue Xuebao, Vol 42, Iss 4, Pp 689-696 (2024)
In the modern civil transport aircraft flight test, flight test practitioners need to constantly improve the ability and reduce flight test cycle as much as possible, considering the relationship between flight test efficiency and flight test safety.
Externí odkaz:
https://doaj.org/article/5519f868aa9b4599903335359f4b3568
Publikováno v:
Aircraft Value News. 3/27/2023, pN.PAG-N.PAG. 1p.
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2023, Vol. 96, Issue 1, pp. 27-33.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-04-2023-0113
Publikováno v:
Journal of Mechanical Engineering, Vol 26, Iss 3, Pp 28-32 (2023)
This paper is dedicated to ensuring the strength of cargo equipment elements of transport aircraft. The strength of rollers of roller conveyors, which are made of standard pressed aluminum tubular profiles or composite tubular elements, is considered
Externí odkaz:
https://doaj.org/article/b75237ab909f4e0fb4f7f73d89033d3b
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2023, Vol. 95, Issue 6, pp. 974-984.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-02-2022-0046
Publikováno v:
Aircraft Engineering and Aerospace Technology, 2023, Vol. 95, Issue 6, pp. 912-925.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/AEAT-03-2022-0081
Publikováno v:
Journal of Mechanical Engineering, Vol 26, Iss 2, Pp 39-45 (2023)
The subject of research in the paper is the process of forming a criterion base to evaluate the effectiveness of carrying out modification changes in a transport category aircraft. The goal is to develop supporting criteria for making decisions regar
Externí odkaz:
https://doaj.org/article/b1747ee090da46cd882d1211d67e0fd1
Publikováno v:
Hangkong gongcheng jinzhan, Vol 14, Iss 2, Pp 129-135 (2023)
The performance software of a domestic civil aircraft used by an airline for many years can obtain satisfactory results in the accuracy of obstacle limited weight calculation, but the calculation time is long. The optimization model is established by
Externí odkaz:
https://doaj.org/article/090e436812cb4ad694abf5a6e816d13b
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