Answer Happy

Maneuvering Performance During Flight G-loading G-loading is calculated using the following Equation 11.3 from (Badick & Johnson, 2022) G= L W Equation 11.3, the G-loading Equation, defines G-loading as the ratio between the maximum load an aircraft can handle and its total weight (Badick & Johnson, 2022). Safety of the flight depends on the aircraft's ability to withstand positive and negative G loads. For instance, to avoid overloading the aircraft structure and causing damage to it. The G required to maintain altitude in a coordinated turn can be calculated using Microsoft Excel table in conjunction with Equation 11.4 from (Badick & Johnson, 2022), G= case Altitude d CL V STALL C -V Ver 5 4 3 2 1 o 70 -1 STALL -2 80 90 100 5000ft 0.8617 1.55 110 56.9 knots -1.25 63.4 knots 157 knots V-G Diagram 120 130 140 150 160 170
Weight (W) Wing Area (5) Cimax Cimin Vstall Vneg-stall G-pos V G-nes V 2250 174 1.55 -1.25 56.9 63.4 0 0 0 -0.5 0 44.83057 3.8 0 -1.52 G+ ف 1 1.5 2 2.5 3 3.5 3.8 56.9 69.68798 80.46875 89.9668 98.55369 106.4502 110.9185 157 157 157 Load Factor Table 3.8 -1.52 -1 -1.5 -1.52 -1.52 -1.52 63.4 77.64882 78.16477 79 80 -1.52 90 3.8 111 3.8 113 3.8 115 -1.52 -1.52 -1.52 120 100 140 3.8 119 -1.52 150 3.8 120 -1.52 157 3.8 130 3.8 140 3,8 150 The maximum positive and negative G-loading for the aircraft is rated at 3.8G and -1.52G respectively. 3.8 157
An aircraft's maneuver speed.Va, is calculated by intersecting its aerodynamic and structural limits. At minimum airspeed, the maneuver speed is the speed where the maximum bank angle can be achieved. When travelling at this speed, minimum and maximum turn radiuses can be realized (Badick & Johnson, 2022). A plane's weight directly affects its maneuvering speed. An aircraft that maintains the calculated maneuvering speed range will not overstress its structure, but it will stall before it reaches the Limit Load Factor. Overspeed will overstress the aircraft's structure and cause it to exceed its Limit Load Factor, causing it to stall. Negative G-load maneuvering speed is 70.143 knots, while positive G-load maneuvering speed is 110.906 knots. The maneuvering speed is calculated using Equation 11.9 from (Badick & Johnson, 2022). Va VSTALL VLLF VA3.8G 56.89349 knots x √3.8-110.90583 knots VAL52G 56.89349 knots x √1.52-70.14301 knots