Bjorn’s Corner: Aircraft drag reduction, Part 14

January 26, 2018, ©. Leeham Co: In the last Corner, we discussed Induced drag after having covered Friction drag and Form drag. These are the main drag components of a subsonic aircraft. As the aircraft flies over Mach 0.5,… Read More

Bjorn’s Corner: Aircraft drag reduction, Part 13

January 19, 2018, ©. Leeham Co: In the last Corner, we described how the boundary layer theory lead to the understanding of Friction drag for aircraft. The mechanisms behind Induced drag was understood about the same time. Once again… Read More

Bjorn’s Corner: Aircraft drag reduction, Part 12

January 12, 2018, ©. Leeham Co: In the last Corner, we described how the theory for the boundary layer was proposed by Ludwig Prandtl, and how this led to an understanding of the source of Friction drag for an… Read More

Bjorn’s Corner: Aircraft drag reduction, Part 11

January 05, 2018, ©. Leeham Co: In the last Corner we described a dominant drag component affecting the Wright Brothers’ Flyer, Form drag. The many wires and braces on the Flyer created separations and a high Form drag was… Read More