International Journal of Aerospace Engineering / 2018 / Article / Fig 2

Research Article

Adaptive Differential Thrust Methodology for Lateral/Directional Stability of an Aircraft with a Completely Damaged Vertical Stabilizer

Figure 2

Engine thrust response at Mach 0.65 and 20,000 feet.

Article of the Year Award: Outstanding research contributions of 2020, as selected by our Chief Editors. Read the winning articles.