Avia 30 - Study guides, Class notes & Summaries

Quiz: Humans as the Challenge & Solution Due Apr 29, 2024 at 11:59pm Points 25 Questions 25 Time Limit 90 Minutes Instructions The quiz: Covers the Learn material from your textbook in Module 6: Week 6. Contains 25 multiple-choice, multiple-choice, and true/false questions. Is limited to 1 hour and 30 minutes. Allows 1 attempt. Is worth 25 points. Question 1 1 / 1 pts What flight is considered the Miracle on the Hudson? United Airlines Flight 232 Germanwings Flight 9525 US...

AVIA 305 Final Exam Questions and Answers Latest Update 2024/2025 Graded A+. The Airplane Flying Handbook describes Medium Turns (20 to 45 of bank) as those in which the angle of bank remains nearly constant. This type of turn demonstrates Selected Answer: Neutral lateral stability • Question 3 2.5 out of 2.5 points If an aircraft that has been disturbed from its equilibrium position has the initial tendency to return to it's original equilibrium position, it is demonstrating Select...

An airplane is towing a glider to altitude. The tow rope is 20° below the horizontal and has a tension force of 300 lb exerted on it by the airplane. Find the horizontal drag of the glider and the amount of lift that the rope is providing to the glider. Sin 20° = 0.342; cos 20 °= 0.940. correct answers Drag: Cos 20° = D/T (Rearrange) D = Cos 20° X Tension D = 0.940 X 300lbs D = 282lbs Lift: Sin 20° = L/T (Rearrange) Lift = Sin 20° X Tension Lift = 0.342 X 300 lbs Lift...

AVIA 305 Final Exam Questions With Answers Latest Update 2024/2025 (Graded A+) The Airplane Flying Handbook describes Medium Turns (20 to 45 of bank) as those in which the angle of bank remains nearly constant. This type of turn demonstrates Selected Answer: Neutral lateral stability • Question 3 2.5 out of 2.5 points If an aircraft that has been disturbed from its equilibrium position has the initial tendency to return to it's original equilibrium position, it is demonstrating Sele...

AVIA 305 Final Exam Questions and Answers Latest Update 2024/2025 | Graded A+. A Normal shock wave will have what effect on velocity and Mach number? Selected Answer: Decrease to subsonic • Question 2 2.5 out of 2.5 points The Airplane Flying Handbook describes Medium Turns (20 to 45 of bank) as those in which the angle of bank remains nearly constant. This type of turn demonstrates Selected Answer: Neutral lateral stability • Question 3 2.5 out of 2.5 points If an aircraft that...

An airplane is towing a glider to altitude. The tow rope is 20° below the horizontal and has a tension force of 300 lb exerted on it by the airplane. Find the horizontal drag of the glider and the amount of lift that the rope is providing to the glider. Sin 20° = 0.342; cos 20 °= 0.940.Drag: Cos 20° = D/T (Rearrange) D = Cos 20° X Tension D = 0.940 X 300lbs D = 282lbs Lift: Sin 20° = L/T (Rearrange) Lift = Sin 20° X Tension Lift = 0.342 X 300 lbs

AVIA 305 Final Exam Questions and Answers Latest Update 2024/2025 | Graded A+. A Normal shock wave will have what effect on velocity and Mach number? Selected Answer: Decrease to subsonic • Question 2 2.5 out of 2.5 points The Airplane Flying Handbook describes Medium Turns (20 to 45 of bank) as those in which the angle of bank remains nearly constant. This type of turn demonstrates Selected Answer: Neutral lateral stability • Question 3 2.5 out of 2.5 points If an aircraft that...

AVIA 305 Test Prep UPDATED Exam Questions and CORRECT Answers An airplane is towing a glider to altitude. The tow rope is 20° below the horizontal and has a tension force of 300 lb exerted on it by the airplane. Find the horizontal drag of the glider and the amount of lift that the rope is providing to the glider. Sin 20° = 0.342; cos 20 °= 0.940. - CORRECT ANSWER- Drag: Cos 20° = D/T (Rearrange) D = Cos 20° X Tension

AVIA 305 Quiz- Maneuvering Performance Answers 2023 AVIA 305 Quiz- Maneuvering Performance Answers 2023

The difference between the CL curves for straight-wing aircraft is that a) the swept wing aircraft has a lower value of CL (max) b) the straight wing aircraft does not fly at as high an AOA for CL (max) c) the swept wing aircraft does not have an abrupt loss of lift at CL (max) d) all of the above d) all of the above