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AVIA 305 Quiz Stability Covers the Learn material from Module 7: Week 7 — Module 8: Week 8. Which of the following may result in decreased lateral stability of a fixed-wing airplane. If an aircraft is rolled into a given bank, released, and continues to roll further into a steeper bank demonstrates The local airspeed…
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AVIA 305 Quiz Airspeed, Airfoils, Lift, and Drag A 22,492 lb. aircraft has a (L/D)max value of 9.5; find its minimum drag. An aircraft is traveling west at an airspeed of 206 knots and is experiencing a crosswind of 19 knots from the north (90). Find the Groundspeed to two decimal places. An aircraft is…
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AVIA 305 Quiz Maneuvering Performance Covers the Learn material from Module 5: Week 5 — Module 6: Week 6. Dynamic hydroplaning Directional control during a crosswind takeoff in a C172 should be maintained with coordinated use of ailerons and the rudder. A steep turn during level flight can be considered any bank angle above: If…
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AVIA 305 Quiz Aircraft Performance Covers the Learn material from Module 3: Week 3 — Module 4: Week 4. As altitude increases, power available from a turboprop engine: (Reference Figure 6.30) Using Figure 6.30, find the velocity for maximum endurance for the airplane at 12,000 lbs. A total drag curve can also be considered a…
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AVIA 305 Test 4 Liberty University AVIA 305 Quiz Aircraft Performance AVIA 305 Quiz Maneuvering Performance AVIA 305 Quiz Airspeed, Airfoils, Lift, and Drag AVIA 305 Quiz Stability In Subsonic flight the air is considered to be A Normal shock wave will have what effect on velocity and Mach number? Aircraft speeds where the airflow…
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AVIA 305 Test 3 Liberty University AVIA 305 Quiz Aircraft Performance AVIA 305 Quiz Maneuvering Performance AVIA 305 Quiz Airspeed, Airfoils, Lift, and Drag AVIA 305 Quiz Stability Which statement is true with respect to Lift Coefficient (CL) and the Effect of Sweepback on Coefficient of Lift – Angle of Attack (AOA) curves. For a…
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AVIA 305 Test 2 Liberty University AVIA 305 Quiz Aircraft Performance AVIA 305 Quiz Maneuvering Performance AVIA 305 Quiz Airspeed, Airfoils, Lift, and Drag AVIA 305 Quiz Stability The thrust available from a jet engine at 35,000 ft altitude compared to that at sea level is If the weight of a jet airplane is increased…
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AVIA 305 Test 1 Liberty University AVIA 305 Quiz Aircraft Performance AVIA 305 Quiz Maneuvering Performance AVIA 305 Quiz Airspeed, Airfoils, Lift, and Drag AVIA 305 Quiz Stability An airplane is operating from an airfield that has a barometric pressure of 28.86 in. Hg and a runway temperature of 20C. Calculate (or find in Table…
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AVIA 305 Research Paper Liberty University The student will submit a 4–6-page research paper on the unique aerodynamic characteristics of his/her favorite aircraft. The paper must adhere to current APA format. The 4–6-page length requirement does not include the title page, abstract, or bibliography. A minimum of 3 sources will be submitted in an Annotated…