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Sung et al., 2012 - Google Patents

Fluidic thrust vector control of supersonic jet using coflow injection

Sung et al., 2012

Document ID
7987893356990081183
Author
Sung H
Heo J
Publication year
Publication venue
Journal of propulsion and power

External Links

Snippet

THRUST-VECTOR control (TVC) systems tend to be progressively implemented in modern aircraft and missiles to improve the slow pitchover and limited maneuverability of the aerodynamic control system [1–3]. A mechanical TVC system moves a nozzle or deflectors …
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