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What is Thrust Vectoring and its applications? Does anyone who can explain it ?
The discussion revolves around thrust vectoring, exploring its definition, applications, and historical context. Participants share insights on various aircraft that utilize thrust vectoring and its implications for maneuverability in aviation and missile technology.
Participants express differing views on the specifics of thrust vectoring in various aircraft, particularly regarding which models utilize it and to what extent. There is no consensus on the historical origins of thrust vectoring, with multiple perspectives presented.
Some participants note the limitations of their knowledge regarding thrust vectoring and afterburner mechanics, indicating a reliance on external sources for detailed information.
Aeronautical engineering students, aviation enthusiasts, and individuals interested in military aircraft technology may find this discussion beneficial for understanding thrust vectoring and its applications.
cronxeh said:Thrust vectoring is directing output stream using nozzles.
Applications? SU-37 has the best thrust vectoring example
http://altnet.ru/~military/avia/istrib/Su-37/Su-37(9).jpg
Those nozzles can move around and direct the exhaust and therefore make sharper and faster turns on an airplane
Another example of thrust vectoring is on F/A-22, and F/A 18 (I think)
cronxeh said:I stand corrected. However, NASA did modify it to make an experimental F-18 HARV
http://www.nasa.gov/centers/dryden/research/HARV/rd.html I'm not sure where I've seen the thrust vectoring F18 but this could be it..
Nenad said:so the after burners do not increase the turbofan rpm, or the turbine rpm. It just combusts and uses the extra exhaust gas as a thrust force, kind of like on a rocket.
Is this correct?
EngTechno said:What is Thrust Vectoring and its applications? Does anyone who can explain it ?
Initial US involvement with the Harrier began in 1957 when Hawker’s revolutionary design was met with disinterest by the British government and a lack of government funding to proceed into development. By that time, the US had conducted extensive research on numerous competitive concepts for V/STOL flight, including aircraft-tilting (tail sitters), thrust-tilting (tilt rotors), thrust-deflection (deflected slipstream), and dual-propulsion (lift-cruise engines) concepts. The simplicity and elegance of the rotatable nozzle vectored-thrust concept of the P.1127 so impressed NASA Langley management and researchers that a formal agreement for cooperative testing was initiated with Hawker under the Mutual Weapons Development Program of NATO.