Airfoil Tank Tops

Description: A schematic depicts an airfoil interacting with undisturbed flow, showing air deflecting upwards and downwards. Below, a formula and two rows of graphs illustrate fluid dynamics, featuring spheres with swirling blue arrows and contour plots with flow lines and numerical axes.

Description: This design features an airfoil or a wing section and its pressure contour. It is a characteristic image from the world of aerodynamics, fluid dynamics, and aerospace engineering. Computers can help simulate the fluid's behaviour around and airfoil but extensive validation is required throguh wind tunnel experiments.

Description: Never forget the main parts of any airfoil with this cool design! Created in the style of the classic engineering blueprints, the airfoil is the basis upon which an aircraft's wing generates lift and is able to stay up in the air. The world of aerodynamics is fun!

Description: A scientific diagram illustrating fluid dynamics. The top shows airflow over an airfoil. The middle section depicts flow patterns around a cylinder at different velocities, including laminar and turbulent flow. The bottom row presents three graphs: a single peak distribution, a multi-peak distribution, and a complex fluctuating waveform.

Description: A boomerang is a thrown tool

Description: A scientific diagram displays fluid dynamics principles with an airfoil and various object shapes interacting with flow lines. It includes an equation involving partial derivatives and a logarithmic function. Three separate diagrams show flow patterns around circular, spiked, and smooth objects, with accompanying graphical representations of flow data.

Description: A scientific diagram illustrating fluid dynamics. The top section shows airflow around an airfoil, with the equation 'P + 1/2 ρv^2 + ρgh = constant' displayed. Below are three diagrams of flow around a cylinder, showing laminar, transition, and turbulent states with associated pressure distribution graphs.

Description: A scientific diagram displaying fluid dynamics concepts. It features an airfoil cross-section with flow lines, a complex partial differential equation, three visualizations of flow around a cylinder at different Reynolds numbers, and three corresponding plots showing pressure (P/P) and velocity (V/P) against spatial variables (Yp, YB, XB). The overall style is monochrome with white lines and text on a black background.

Description: A black background displays a diagram illustrating aerodynamic principles. A gray airfoil shape is shown with blue arrows indicating airflow. Text labels identify 'LOW PRESSURE AREA' above the airfoil and 'POSITIVE PRESSURE AREA' below. A red arrow labeled 'LIFT VACUUM' points upwards.

Description: Airfoil in the wings of airplane works based on Bernoulli's principle. Airfoil designed to have more length on the top side, thus the wind that split during its collision with the airfoil needs to travel faster on the top side compared to the bottom side. This will make the pressure on the bottom side higher than the top side of the airfoil, resulted in the generation of lift force that makes the airplane fly. As the angle of airfoil increased, the void appeared on the tail of airfoil creating pressure drop on this area and the air flowing in turbulence. If this condition continues, the pressure on the front of airfoil builds up and the rear dropped, resulting in more drag force compared to the generated lift, and turning it to stall.