As the angle of attack is increased on a high-performance airfoil, a small amount of separation occurs near the leading edge. This separation causes the boundary layer to transition from laminar to ...
Considering the characteristics of large slenderness ratio structure, it is reasonable to simplify the dynamics of a HALE aircraft as the plunge, pitch, and flap motions of a planar airfoil. The ...
In Part 2, we discussed Learjet’s research into improving the stall characteristics of its aircraft. Bombardier’s Clinton E. Tanner, senior technical advisor of flight sciences, points out that ...
Some results have been hidden because they may be inaccessible to you
Show inaccessible results