Results 11 to 20 of about 5,057 (307)

Numerical Investigation on the Thrust Vectoring Performance of Bypass Dual Throat Nozzle

open access: yesEnergies, 2023
Modern aircraft and missiles are gradually integrating thrust vector control systems to enhance their military capabilities. Bypass Dual-Throat Nozzle (BDTN) control is a new fluidic thrust vectoring technique capable of achieving superior performance ...
Saadia Afridi   +6 more
doaj   +1 more source

Thrust vectoring systems [PDF]

open access: yes8th Electric Propulsion Conference, 1970
The design, fabrication, and testing of thrust vectorable ion optical systems capable of controlling the thrust direction from both 5- and 30-cm diameter ion thrusters is described. Both systems are capable of greater than 10 deg thrust deflection in any azimuthal direction.
H. KING, D. SCHNELKER
openaire   +1 more source

Differential Throttling and Fluidic Thrust Vectoring in a Linear Aerospike

open access: yesInternational Journal of Turbomachinery, Propulsion and Power, 2021
Aerospike nozzles represent an interesting solution for Single-Stage-To-Orbit or clustered launchers owing to their self-adapting capability, which can lead to better performance compared to classical nozzles.
Michele Ferlauto   +3 more
doaj   +1 more source

A novel divertless thrust vectoring nozzle using the countercirculation aerodynamic effect: Maximal Aerodynamic Yaw Actuator-MAYA [PDF]

open access: yesINCAS Bulletin, 2011
During the second half of the 20th century, Henri Coanda had extensively studied theCoanda effect and also it’s application for high lift devices that use –in one way or another- supercirculation. A previous work has been done for using the Coanda effect
Valeriu DRĂGAN
doaj   +1 more source

Fluid Dynamics of Thrust Vectorable Submerged Nozzle [PDF]

open access: yesFluids, 2021
A numerical simulation of the gas-dynamic processes in the thrust vectorable nozzle of the solid rocket motor is considered. Construction of a geometric model and a generation of computational mesh, and reconstruction of model and mesh at each time step are discussed.
Denisikhin, Sergey   +2 more
openaire   +3 more sources

Investigation of active flow control of jet deflection rate in passive secondary flow thrust vectoring nozzle

open access: yesAIP Advances, 2022
Jet deflection rate is an essential index in the research of thrust vector control technology. The vectoring deflection of the jet is an unsteady flow.
Shaoqing Chi   +3 more
doaj   +1 more source

Numerical Study on Rod Thrust Vector Control for Physical Applications

open access: yesInternational Journal of Aerospace Engineering, 2021
Mechanical thrust vector control is a classical and significant branch in the thrust vector control field, offering an extremely reliable control effect.
Dong Li, Kexin Wu
doaj   +1 more source

Influence of Bypass Location on Two-Dimensional Shock Vectoring Nozzle

open access: yes气体物理, 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.
Bo-wen SHU   +4 more
doaj   +1 more source

Determination of Optimum Parameter Space of a Fluidic Thrust Vectoring System based on Coanda Effect Using Gradient-Based Optimization Technique [PDF]

open access: yesJournal of Applied Fluid Mechanics, 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.
E. Kara, D. F. Kurtuluş
doaj   +1 more source

Effect of Thrust Vectoring Technology on Taking-Off Performance of Hypersonic Vehicle

open access: yesMATEC Web of Conferences, 2015
Owing to the high sweep angle and the slender structure, much less taking-off lift is produced by the horizontal taking-off hypersonic vehicle compared with general aircrafts. This paper aims at introducing the thrust vectoring technology into the taking-
Wu Yushan   +3 more
doaj   +1 more source

Home - About - Disclaimer - Privacy