Corpus ID: 13344436

A 98-37266 HIGH SPEED , LOW ANGLE-OF-ATTACK PNEUMATIC VORTEX CONTROL . AJAA-98-4449

@inproceedings{Valasek2001A9H,
  title={A 98-37266 HIGH SPEED , LOW ANGLE-OF-ATTACK PNEUMATIC VORTEX CONTROL . AJAA-98-4449},
  author={J. Valasek and Lawrence A. Walchli},
  year={2001}
}
Forebody pneumatic vortex control has previously been demonstrated through full-scale flight test to be effective for directional control of aircraft at low Mach number and high angle-ofattack flight conditions. The objective of the present research was to investigate the suitability of two-axis (wing, and vertical tail) pneumatic vortex lateral/directional control of a current fighter-type aircraft at high Mach number and low angle-ofattack flight conditions. The pneumatic effectors were… CONTINUE READING

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