Technical Questions Flashcards
What is a Yaw Damper?
Servo that smoothly automates rudder pedals to maintain coordination.
Prevents Dutch Roll. Oscillating turns with opposite roll and yaw.
What Factors affect V1
Weight, pressure altitude, temperature, wind, runway length, runway slope, runway condition, flaps, equipment in use (thrust reverse, icing, ect)
What are N1 and N2?
N1 = Low pressure compressor, how power is set. Intake.
N2 = high pressure compressor, initial power on startup, shows power to systems. Engine core.
What systems are powered by hydraulics?
Flight controls, landing gear, brakes, flaps, spoilers, thrust reverse
What is RVR?
Runway Visual Range = horizontal distance pilot can see down the runway. 3 sensors, reported in feet.
What are some things that effect stall speed?
Load Factor, Weight, CG, Flaps/Slats, wing contamination
How do you increase the stall speed of an airfoil?
Increase Load Factor/AoA, forward CG, Flaps up, wing contamination
Effects of Forward CG
increase longitudinal stability, increase stall speed, less fuel efficient
Effects of Aft CG
Decrease longitudinal stability, decrease stall speed, more fuel efficient
How does altitude affect your stall AOA?
Air density decreases, lift decreases and stalls at a lower AOA
Why does stall speed increase with altitude?
Air density decreases, airfoil requires more laminar flow (speed) over the wing to create the same amount of lift
Why is it bad for a wing to stall at the wingtip first?
Roll control is lost first
What do flaps do and how do they work?
High lift device, increase wing camber, decreases stall speed, increase drag. Allows for lower AoA on approach without increasing speed.
What is a Mach Number?
Speed of an object in relation to speed of sound
What is Critical Mach?
When any point on the aircraft reaches the speed of sound (usually just below mach 1.0)
How are Critical Mach, Stall speed, and Altitude related?
Stall speed gets faster and speed of sound is slower with altitude. They converge on each other in the coffin (Q) corner. Can have stall buffet or overspeed buffet.
What happens to IAS with increase in altitude?
Decreases
What happens to TAS with increase in altitude?
Increases (air is less dense/less drag)
What happens to Mach Number with increase in altitude?
Mach number changes with temperature: Colder (generally higher altitude) = lower speed of sound = higher mach number
Why does an aircraft lose airspeed in a turn if thrust is not increased?
Vertical lift is traded for horizontal requiring an increase in AOA to maintain altitude. Increase in AoA reduces speed requiring power to compensate.
Swept wing advantages? Particularly jet aircraft?
Increases critical mach number, by delaying wave drag (supersonic shockwaves).
What are the stall characteristics of a swept wing?
Wing tip stalls first, higher AoA at low speeds required if flaps/slats ect not used.
Types of Drag
Induced and Parasitic (Parasitic has skin friction, form, interference). High speed has wave drag.
What happens to the speed of sound as altitude increases?
Speed of sound decreases with a decrease in temperature (standard lapse rate would be colder as altitude increases)
What is Mach Tuck and how is it counteracted?
Shockwaves cause center of pressure to move aft requiring increase in AoA. When shockwaves reach a critical level, elevator effectives is lost due to lack of smooth air flow causing a nose dive. Counteracted by stabilators and vortex generators.
What does critical Mach have to do with Mach tuck?
When critical mach is reached shockwaves begin to form. The lower critical mach is the sooner mach tuck is likely to occur.