Joby Aviation’s Post

Wings are equipped with different extensions, such as slats and flaps, to enhance their performance during critical flight phases. Slats improve airflow at high angles of attack and low airspeeds, delaying the stall, while flaps increase lift at low speeds by increasing wing area. These extensions are retracted when not needed to reduce aerodynamic drag. https://aviationplanet.in/

Airplane Yaw Control and Forces During a Sideslip ✈️ - Sideslip Angle: The angle between the airplane's direction of travel and its longitudinal axis 🛬. - Thrust: The forward force produced by the airplane's engines 🔄. - Thrust Yawing Moment: The turning effect caused by the thrust during sideslip 🔁. - Rudder Deflected: When the rudder is moved to counteract the sideslip 🛞. - Rudder Side Force: The force generated by the deflected rudder pushing the tail sideways 🌬️. - Rudder Yawing Moment: The rotational force created by the rudder to steer the plane 🛫. - Sideslip Yawing Moment: The rotational force due to sideslip that affects the airplane’s direction 🌐. - Side Force Due to Sideslip: The force that pushes the airplane sideways due to the sideslip angle ⬅️. These forces and moments are crucial for controlling the airplane’s yaw and ensuring stable flight! 🌍✈️

It seems the same, but there was a lot of effort to generate this chart. The black line, at the bottom chart, represents the vertical flight profile of a medium range aircraft with one-engine inoperative at a constant speed of 250 KIAS. As can be seen, the vertical profile does not clear the obstacles, thus dictating the need for an engine-out procedure. I am planning now to refine the flight trajectory, including the drag from high-lift configuration, the effect of turns and the acceleration from V2 to VFS at 1500 ft AGL. Another thing I am planning to do is to generate the optimum horizontal profile, from the Dijkstra's algorithm, without sharp turns.

Check Flight Complete! A critical step to validate platform assembly, configuration and maintenance status. Winds are always a factor. The Swoop Aero handled nominally in 10-15 mph with gust over 20 mph. Watch how it maneuvers to land on the target.

Unlock The Power of Precision: Your Ultimate Mavic 3 Thermal Setup Guide Ready to get your Mavic 3 Thermal airborne? Follow these simple steps to ensure a smooth setup and takeoff: 1. Charge the Flight Battery: Ensure it's fully charged, which takes about 1 hour and 20 minutes. 2. Unfold the Arms: Start with the front arms, then unfold the rear arms. 3. Remove the Gimbal Protector: Take off the protector from the camera to prepare it for use. 4. Attach the Propellers: Secure them onto the arms for stable flight. 5. Activate the Remote Controller Battery: Charge the remote controller to activate its battery. 6. Prepare the Control Sticks: Remove the sticks from their storage slots on the remote controller and screw them into place. 7. Unfold the Antennas: Extend them to ensure optimal signal reception. With these steps, you're all set to take your Mavic 3 Thermal to the skies! Happy flying! 🚁

"Wingtip devices can be used to alleviate gust loads and reduce the risk of intense aerodynamic forces near the wingtip, enhancing the aircraft's overall stability and safety." https://lnkd.in/gFraBBVT

Increasing Lateral Stability Wing Placement - Low-wing: Less stable laterally because the center of gravity is above the wing. - High-wing: More stable laterally as the center of gravity is below the wing. Dihedral - Dihedral angle: Wings angled upward increase stability. - Sideslip: Causes more lift on the lower wing, creating a rolling moment that corrects the aircraft's position. - Result: Helps the aircraft return to level flight during sideslips.

An airplane can move in three primary directions, each aligned with a three-dimensional axis: the longitudinal axis (front to back), the lateral axis (wing to wing), and the vertical axis (top to bottom). The movements associated with these axes are: 📌Roll: Longitudinal Axis- Roll involves rotation around the longitudinal axis, tilting the wings up or down to facilitate left or right turns. This movement is controlled by the ailerons on the wings. 📌Yaw: Vertical Axis- Yaw is the rotation around the vertical axis, altering the direction the nose of the plane faces (left or right). This is managed by the rudder at the tail of the aircraft. 📌Pitch: Lateral Axis- Pitch entails movement around the lateral axis, causing the nose of the plane to rise or fall to change altitude. Elevators at the tail control this movement.

Figure (a) illustrates a head-on perspective of an airplane with dihedral wings, where the wings are angled upward relative to the horizontal plane. If a disturbance causes one wing to dip below the other, as shown in Figure (b), the lift vector tilts, and a component of the aircraft's weight acts inward, inducing a lateral movement in that direction. Due to the dihedral angle, the lower wing—being more aligned with the free-stream airflow—experiences a higher angle of attack compared to the raised wing, generating greater lift. This difference produces a net force and moment that work to restore the wings to a level position, reducing the bank angle, as depicted in Figure (c).

Let's start by visualizing the facts imposed on the aerodynamic surface.