Aerodynamics Assessment Welcome, You are about to take up the Aerodynamics Assessment. Please take note of the following before you take the assessment. This assessment is timed for 60 Mins and auto submit. Scores and correct answer will be displayed after taking up the assessment. You can only take the assessment twice so make sure you have a strong internet connection. All questions are required to have an answer. This assessment is composed of 10 items multiple choice type of question. Always remember: THINK, CHECK AND SUBMIT. If you have any concern, please feel free to contact us. E-mail Address: assessment@flightwingsaviation.com Facebook Page: www.facebook.com/flightwingsaviation GOODLUCK! Email Adress LMS USERNAME FULL NAME CLASS SECTION/SCHEDULE (FRI-AM, FRI-PM, SAT-AM, SAT-PM, SUN-AM, SUN-PM, ONLINE) 1. Yaw is defined as the movement of the longitudinal axis about which axis? A. LateralB. LongitudinalC. VerticalD. Horizon A B C D 2. The net aerodynamic forces can be resolved into what two component forces? A. Lift and dragB. Weight and dragC. Thrust and dragD. Dynamic and static pressure A B C D 3. What must you do to remain in formation as your aircraft takes on fuel (increasing weight) from the tanker that is maintaining a constant altitude and true airspeed? A. Maintain a constant AOA and TASB. Decrease AOA and increase TASC. Increase AOA and maintain constant TASD. Increase AOA and TAS A B C D 4. High density altitude will: A. Decrease the power produced by an engine and increase the thrust produced by the propeller or jetB. Increase the power produced by an engine and increase the thrust produced by the propeller or jetC. Decrease the power produced by an engine and decrease the thrust produced by a propeller or jetD. Increase the power produced by an engine and decrease the thrust produced by the propeller or jet A B C D 5. All motion or changes in aircraft attitude occurs about which position? A. Aerodynamic centerB. Center of pressureC. Center of gravityD. The cockpit A B C D 6. For a given altitude, what are the properties of the input provided by the static pressure port in the pitot-static system? A. The static pressure value will vary with changes in aircraft true airspeed (TAS)B. The static pressure value will vary with changes in aircraft angle of attack (AOA)C. The static pressure value will vary with changes in aircraft weight D. The static pressure value will vary with changes in atmospheric ambient static pressure and altitude A B C D 7. Two planes leave manila for southern city, a distance of 900 km. plane A travels at a ground speed of 90 kph faster than the plane B. Plane A arrives in their destination 2 hours and 15 minutes ahead of plane B. what is the ground speed of plane A? A. 205 KPHB. 315 KPHC. 240 KPHD. 287 KPH A B C D 8. When the value on the aircraft indicated airspeed (IAS) indicator equal the aircraft true airspeed (TAS) A. When static pressure at aircraft altitude is less than static pressure at sea level, on a standard dayB. When static pressure at aircraft altitude is greater than static pressure at aircraft sea level, on a standard dayC. When static pressure at aircraft altitude equals static pressure at sea level, on a standard dayD. When static pressure at aircraft altitude equals density at sea level, on standard sea level A B C D 9. An aircraft is climbing at a constant 350 KIAS. What change occurs in Mach number as altitude increases? A. Mach number increasesB. Mach number decreases C. Mach number remains constantD. There is no Mach number at this speed A B C D 10. Due to friction along the connections of engine components such as gears, lobes, shafts and any mechanical transmission would tend to A. Reduce the power being transmittedB. Increase the power being transmittedC. Multiply the power being transmittedD. Nothing happen to the power being transmitted A B C D 1 out of 1