Fluidic thrust vectoring and control refer to a suite of aerodynamic techniques that achieve directional control of engine thrust by modulating the flow field through the injection of secondary ...
Fluidic thrust vectoring nozzles represent a promising approach in aerospace propulsion, utilising the controlled injection of secondary flows to manipulate the primary exhaust stream. This innovative ...
National Security Journal on MSN
The X-44 Manta Has a Message for Every Air Force on Earth
The X-44 MANTA was a “radical” 1990s Lockheed Martin concept for a “tailless F-22,” which would have used 3D thrust vectoring ...
Marotta’s TVC system offers advanced control by gimbaling the rocket motor’s nozzle, enhancing the missile’s navigation and precision. This actuator-driven design ensures precise trajectory ...
National Security Journal on MSN
Frankenstein F-22 Raptor: The X-44 Manta Stealth Fighter Haunts My Dreams
Key Points and Summary – The X-44 MANTA was a radical, tailless derivative of the F-22 Raptor that promised extreme stealth, ...
Tranche 2 Eurofighter Typhoons will be delivered with upgraded control units for their Eurojet EJ200 engines designed to support the future introduction of a thrust-vectoring capability. The digital ...
Barnstorming is rare at aerospace trade shows these days, but the thrust-vectoring RSK MiG-29M OVT fighter has rekindled the air display spirit with an arresting flying demonstration. The double ...
ATK's TVECS system is the latest innovation in controls technology to be successfully demonstrated. ATK designed and qualified the digital field programmable gate array (FPGA)–based TVECS hardware and ...
There’s a good chance you already saw SpaceX’s towering Starship prototype make its impressive twelve kilometer test flight. While the attempt ended with a spectacular fireball, it was still a ...
ZHUHAI, China—An AVIC-owned J-10B testbed demonstrated in a Nov. 6 flying display showed China’s new mastery of extreme aerial maneuverability aided by an experimental thrust vectoring control system.
In view of the control effects of fluidic thrust vector technology for low-speed aircraft at high altitude/low density and low altitude/high density are studied. The S-A model of FLUENT software is ...
Some results have been hidden because they may be inaccessible to you
Show inaccessible results