An Improved Fluidic Thrust Vector Control Device for Nozzles With Non-Circular Geometries

FLUIDIC THRUST VECTOR CONTROL DEVICE FOR COMPLEX NOZZLE GEOMETRIES SUITABLE FOR

• Engine exhaust nozzles with non-circular exit geometries
• Operating at high subsonic Mach numbers of 0.7-0.9
• Pre-fixed angled twin deflector plates of device occupy very less space

• Defence
• Aerospace
• The global thrust vector control market is projected to reach approximately USD
  23.83 billion by 2031, growing at a CAGR of over 8.7%

• Needs minimum mass flow rates of approximately 1.33% and 5.5%to achieve
  primary jet deflections in of 7oin yaw and 13opitchplanes
• Capable of controlling the direction of the exhaust jet in both pitch and yaw using
  secondary injection around the periphery of the primary nozzle exit plane
• Reduce aircraft after body signature thereby improving stealth capability of the
  aircraft
• Not manipulate flow inside the nozzle
• Free from any mechanical actuators
• Lower cost and compact design