Rising speed increases dynamic pressure, which is ½ times density times velocity squared. Both lift and drag depend on this dynamic pressure: lift is proportional to ½ ρ v^2 S C_L and drag is proportional to ½ ρ v^2 S C_D. So when velocity goes up, and the wing’s lift and drag coefficients don’t drop due to a change in angle of attack or other conditions, both forces rise with v^2. In short, faster flight increases both lift and drag (under typical conditions with the coefficients held constant at a given angle of attack).

Bleed air for this system comes from a crossing (cross-bleed) manifold, not from a single engine port. The crossing manifold is a shared distribution duct that collects bleed air from one or more engine compressor bleed ports (and sometimes the APU) and routes it to the pneumatic/air system through control valves. This arrangement allows the system to be supplied from whichever engine is available or to start an engine using bleed air from the other engine, by crossfeeding through the manifold. External air intake isn’t bleed air, and cabin exhaust isn’t a source of bleed air. The key idea is that the crossing manifold serves as the source/distribution point for the system’s bleed air, enabling flexible, cross-bleed operation.

The tail rotor’s job is to counteract the torque produced by the main rotor and to provide yaw control. When the main rotor spins, the fuselage tends to rotate in the opposite direction. The tail rotor generates thrust to balance that torque, and by varying its thrust, the pilot can rotate the helicopter’s nose to change heading. Lift comes from the main rotor, not the tail rotor. The tail rotor doesn’t supply fuel, which comes from the engine’s fuel system, nor does it handle navigation lights, which are separate avionics.

Drag is the resistive force opposing motion through air. As airspeed increases, the air’s dynamic pressure rises, boosting the forces that generate drag. There are two main parts: parasitic drag (from friction and form resistance on surfaces) grows roughly with the square of speed, while induced drag (from wingtip vortices) decreases with speed. In typical flight regimes, parasitic drag becomes the dominant contributor at higher speeds, causing the total drag to rise as you go faster. So the best answer is that drag increases when airspeed is increased.

Tiltrotor flight relies on three main modes that cover vertical lift, a smooth transition, and efficient forward flight. Vertical takeoff and landing uses the rotors oriented to push air downward, giving lift straight up so the aircraft can hover, lift off, and land without a runway. This capability is what makes tiltrotors unique: they can start from a standstill in the air, then transition to forward flight. As flight progresses, the nacelles tilt toward the front to enter conversion mode, blending lift and thrust to move from vertical to horizontal flight. Finally, in airplane mode the rotors point forward to act mainly as propellers, maximizing speed and efficiency in cruise. So, describing vertical takeoff and landing highlights one of the foundational modes that enable the tiltrotor to operate like a helicopter at low speeds and then like an airplane at higher speeds.