PPT-Aerodynamic Forces

Lift and Drag Lift Equation Coefficient of Lift C l Determined experimentally Combines several factors Shape Angle of attack Lift Direction of Flight             Alternate format. Aerodynamic forces generate a twisting moment which cause the gyroscope to precess and to move on a circular path Let us examine the forces acting on a boomerang of radius The centre of the boomerang is moving at a constant forward speed and the bo By:. Amr. . Malhis. Shadi. . Qazza. Odai. . Amira. Omar Abu . Ghdaib. Supervisor:. Dr.Ramez. Al-Khaldi . Content. Project overview. Today, our energy system is based on motion of the cars over the bump that will concentrated on an aerodynamic energy which consist in every city in the world due to the daily increasing in cars amount.. Define Static stability.. Define Dynamic stability.. Stability in an aircraft affects . what . two . aspects of an aircraft.. Define Lateral stability.. Describe the effect of wing dihedral.. Warm-Up – . Background. Flapping Micro Air Vehicles (FMAVs) as the most intriguing type of MAVs family have obtained a great interest due to their outstanding efficiency and maneuverability. The flapping wings can generate both lift and thrust for an available flight. With onboard cameras and sensitive devices, these radio-controlled FMAVs are capable to implement tasks of surveillance, exploration and rescue. The inherent low Reynolds and unsteady aerodynamics caused by flapping motion results an uncomfortable aerodynamic behavior, conventional aerodynamic theories and analysis methods are no longer applicable on FMAVs. Ultimately, it is always essential to offer the designers and engineers a clear picture about the overall aerodynamic knowledge and useful tool to organize the FMAVs for specific mission objective and flight envelop.. :. CL increases with an increase in AOA, at some point the CL peaks and then begins to drop . off. This . peak is called . ____________.. The wing root reaches its critical AOA . _____ . making the stall progress . Background. The separated wake at the base of cylindrical bodies presents a number of challenges to aerodynamic designers dealing with similar geometries, such as in missiles or rocket launchers, due to the unsteady and three-dimensional character of the wake.. Overview. Streamline Patterns Review. Pressure Patterns. Understanding how lift is Generated. Streamline Review. Streamline Definition. A streamline is a path traced out by a mass less particle moving with the air flow.. FRAP-7S. Unsteady 3-D . flowfield. measurements. High flow acceptance angle. High sensitivity. Non-isotropic turbulence. Fully compatible with . LSc’s. turnkey measurement system. . The Fast-Response . Lift and Drag. © 2011 Project Lead The Way, Inc.. Aerospace Engineering. Lift Equation. Coefficient of Lift, . C. l. Determined experimentally. Combines several factors. Shape. Angle of attack. Lift. What . are t. he . subcomponents of an . airplane? . What . is the basic structure of an . aircraft? . What is . designed to withstand all aerodynamic . forces. ?. What . is t. he . primary function of an aircraft electrical . If an aircraft climbs with no change in the power setting – what happens to airspeed?. Additional . _____ . is required to maintain the same airspeed as in level . flight, when an aircraft climbs. . Neal E. Joslyn. Christopher W. Roberson. Objective. Current State. : Little is known about the effects of dimples on the aerodynamics of bicycle frame tubes. Research Question. : Determine whether a dimpled bicycle frame is more aerodynamic then a smooth one.. Equations of Motion from Chap 3. External Forces and Moments. Gravity Force. above static pressure. below static pressure. Airfoil Pressure Distribution. Aerodynamic Approximation. Control Surfaces - Conventional. © 2011 Project Lead The Way, Inc.. Aerospace Engineering. Lift Equation. Coefficient of Lift, . C. l. Determined experimentally. Combines several factors. Shape. Angle of attack. Lift. Direction of Flight.