Zobrazeno 1 - 10
of 1 256
pro vyhledávání: '"Thrust vectoring"'
Publikováno v:
气体物理, Vol 8, Iss 5, Pp 19-27 (2023)
Fluidic thrust vectoring technology can provide good stealth performance and longitudinal maneuvering moment for supersonic tailless configurations, with advantages of fast response and light weight. The bypass shock vectoring nozzle does not need to
Externí odkaz:
https://doaj.org/article/c8d94fbdde1248549040d652502c4d0f
Autor:
E. Kara, D. F. Kurtuluş
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 16, Iss 10, Pp 1974-1988 (2023)
In the realm of aviation, jet propulsion systems serve to provide enhanced maneuverability and to make sure that the aircraft thrust is accurately and precisely regulated during take-off and landing operations. The movement of aerodynamic control sur
Externí odkaz:
https://doaj.org/article/7a71ea1b91c34919b96099021f280af5
Publikováno v:
Actuators, Vol 13, Iss 6, p 228 (2024)
Autonomous underwater vehicles (AUVs), as primary platforms, have significantly contributed to underwater surveys in scientific and military fields. Enhancing the maneuverability of autonomous underwater vehicles is crucial to their development. This
Externí odkaz:
https://doaj.org/article/74ec3d398c1b4e2c83a91dc7c2b3e8cb
Publikováno v:
Aerospace, Vol 11, Iss 5, p 369 (2024)
Fluid thrust vectoring (FTV) control has obvious advantages in structural quality and stealth performance because of its fast response and light weight. However, improving FTV vector performance will cause a loss in engine performance due to the need
Externí odkaz:
https://doaj.org/article/860eaa68c6d646969f75bf7a9345c39d
Publikováno v:
Bulletin of the Polish Academy of Sciences: Technical Sciences, Vol 72, Iss 2 (2023)
The aim of the study described herein was to design, construct and test a demonstrator of a system to control the direction of the resultant thrust vector of a rocket motor to be used in short range anti-tank missiles with a mass of up to 15 kg. The
Externí odkaz:
https://doaj.org/article/dce09bcd928c466c9aad2e30b3775a58
Publikováno v:
Aerospace, Vol 10, Iss 12, p 978 (2023)
This research developed a pressure-based thrust vectoring angle estimation method for fluidic thrust vectoring nozzles. This method can accurately estimate the real-time in-flight thrust vectoring angle using only wall pressure information on the inn
Externí odkaz:
https://doaj.org/article/9594ca9e96be4206a2dd82a35201b5b6
Akademický článek
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Akademický článek
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Autor:
Saadia Afridi, Tariq Amin Khan, Syed Irtiza Ali Shah, Taimur Ali Shams, Khawar Mohiuddin, David John Kukulka
Publikováno v:
Energies, Vol 16, Iss 15, p 5721 (2023)
Thrust vectoring innovations are demonstrated ideas that improve the projection of aerospace power with enhanced maneuverability, control effectiveness, survivability, performance, and stealth. Thrust vector control systems following a variety of con
Externí odkaz:
https://doaj.org/article/aeb3de2d757f4b2bbd591b25da39a56a
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 15, Iss 4, Pp 1137-1153 (2022)
Dual-throat Nozzle (DTN) is known as one of the most effective approaches of fluidic thrust-vectoring. It is gradually flourishing into a promising technology to implement supersonic and hypersonic thrust-vector control in aircrafts. The main objecti
Externí odkaz:
https://doaj.org/article/f19b77c2a978416cb569eeef4d88bff4