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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

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12 pages

Written in 2024/2025

Grade A+

STANFORDGRADESS

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...

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9 pages

Written in 2023/2024

Grade A+

SirAnton

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 Low speed stall will start at the wing's trailing edge a) where C1/C2 is a minimum b) where C1/C2 is a maximum c) at the root for a swept wing d) at the wingtip for a st...

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9 pages

Written in 2023/2024

Grade A+

WIZGrades

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

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12 pages

Written in 2023/2024

Grade A+

WIZGrades

The equation Ta = Q (V2 - V1) shows thatyou can get more thrust from a jet engine by using water injection. you can get more thrust from a jet engine by decreasing the exhaust pipe area. Q in Ta = Q (V2 - V1) is the mass flow (slugs/sec). The mass flow depends onthe cross‐ sectional area of the turbojet engine inlet. the engine inlet velocity. the density of the air at the same point.

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5 pages

Written in 2023/2024

Grade A+

WIZGrades

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...

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10 pages

Written in 2023/2024

Grade A+

STUDYLAB2023

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...

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10 pages

Written in 2023/2024

Grade A+

STUDYROOM2026

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

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9 pages

Written in 2023/2024

Grade A+

STANFORDGRADESS

The equation Ta = Q (V2 - V1) shows thatyou can get more thrust from a jet engine by using water injection. you can get more thrust from a jet engine by decreasing the exhaust pipe area. Q in Ta = Q (V2 - V1) is the mass flow (slugs/sec). The mass flow depends onthe cross‐ sectional area of the turbojet engine inlet. the engine inlet velocity. the density of the air at the same point.

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5 pages

Written in 2023/2024

Grade A+

STANFORDGRADESS

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

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12 pages

Written in 2023/2024

Grade A+

STANFORDGRADESS

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

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11 pages

Written in 2023/2024

Grade A+

VEVA2K

AVIA 305 Quiz 3 with pictures

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15 pages

Written in 2021/2022

Grade A

noneya