By Gerhard Lang
Common Dynamics F-16 «Fighting Falcon»
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Example text
During the second step, the vectored fighter may roll about the velocity vector to disengage, and/or yaw-vector its nose for starting the second part of a ISO-degrees turn-back maneuver (cf. Lecture II). The final step of such 'nominal' maneuvers involves unloading and acceleration to regain the initial speed/energy level. 9 Low or High Load Factors During Post-Stall Maneuvers by Vectored Aircraft: Intuiton vs. Physics The lift coefficient as well as the effectiveness of all aerodynamic control surfaces are drastically reduced during vectored, rapid-nose-pointing, high AoAlPost-Stall maneuvers (Fig.
In an "energy" fight, the objective is to gain an energy advantage, and, then, at an appropriate time, to trade that energy advantage for position. According to Hodgkinson, Skow, Ettinger, Lynch, Laboy and Chody of Eidetics International and Cord of AFWALlFIGC, Wright Patterson AFB, USAF (184), an "angles" pilot tactician maneuvers his aircraft so that a snapshot opportunity presents itself before he himself has spent his energy. Consequently, a typical "angles" maneuver is to use altitude to sustain the time the aircraft spends close to the comer speed, so that the "angles" tactician can maintain a small tum radius and a high tum rate, thus achieving a snapshot.
Low observability until WVR (Within Visual Range), the technology levels of EW systems and of helmetsight-aiming-systems on both sides, combat-management methodology/systems used, the varying technology limits of all-aspect missiles, the methodology to evade a missile launched previously by a now-destroyed opponent, fighter-strike missions, etc. 5). 6. High-aspect-ratio, split-type, yaw-pitch-roll, vectoring nozzles, have the potential of replacing the horizontal and vertical tails of existing fighter aircraft.
General Dynamics F-16 «Fighting Falcon» by Gerhard Lang
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