Write 7 page essay on the topic Prediction of stall on an aircraft.Stall speeds change with angle of bank, configuration and any changes in gross weight. Furthermore, an aircraft will stall at a highe

Write 7 page essay on the topic Prediction of stall on an aircraft.

Stall speeds change with angle of bank, configuration and any changes in gross weight. Furthermore, an aircraft will stall at a higher speed with flaps retracted than with them extended. The phenomenon of stall is shown in the figure below:-

Stall occur due to a number of reasons and can thus be divided into a number of types1 like power off stalls (also called approach-to-landing stalls, practiced by pilots to simulate normal approach-to-landing conditions and configuration), Power-on stalls (also known as departure stalls, practiced by pilots to simulate takeoff and climb-out conditions) and Accelerated stalls (experienced at higher-than normal airspeeds due to applying abrupt or excessive controls to aircraft and may occur in steep turns, pullups or other abrupt changes in your flight path.).

Many aircraft in Flight Sim use a stall indicator to alert you when the airflow over the wing(s) approaches a point that lift cannot be sustained. The stall indicator is part of aircraft for a reason so no one should ignore it.

Setup a numerical optimization procedure that can be useful to the aerodynamicist in the rapid design and development of high-lift system configurations and that can also provide derivative information regarding the influence of various design parameters (gap, overlap, slat and flap deflection angles, etc.) on the performance of the system.

The variables that describe the relative element positioning can be used as design variables. These variables include flap and slat deflection angles, gaps, overlap, shapes of each of the elements and many more depending on method used2. Like in Continuous Adjoint Method, variables are flow-field variables and the physical location of the boundary. Then the governing equation which expresses the dependence of these variables can be written in flow field domain in form of partial differential equations. After introducing a Lagrange Multiplier and solving adjoint equations and applying boundary