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AVIT 323 FINAL EXAM WITH ALL CORRECT & 100% VERIFIED ANSWERS|ALREADY GRADED A+

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AVIT 323 FINAL EXAM WITH ALL CORRECT & 100% VERIFIED ANSWERS|ALREADY GRADED A+

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CAM - Certified Aviation Manager
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CAM - Certified Aviation Manager









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Institución
CAM - Certified Aviation Manager
Grado
CAM - Certified Aviation Manager

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Subido en
22 de julio de 2025
Número de páginas
6
Escrito en
2024/2025
Tipo
Examen
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AVIT 323 FINAL EXAM WITH ALL CORRECT & 100%
VERIFIED ANSWERS|ALREADY GRADED A+
What's the difference between an airfoil section and a wings platform? Correct answer-An airfoil
section is a side-view of the wing, amd the wing's planform is a top down view

What is the difference between mean camber line and the chord line? Correct answer-Mean
camber: Divides an airfoil section in half between then upper and lower cambers
Chord line: A straight line from the leading edge to the trailing edge

What are the two characteristics of a laminar flow boundary layer? Correct answer-- Good for high
speeds
- Leaves the wing surface at low speeds

Calculate the potential energy of an Archer weighing 2,500lbs if it is 0.5ft above the ground Correct
answer-1250lbs

Law of Conservation of Energy Correct answer-Energy cannot be created or destroyed

The amount of yawing moment that the rudder can generate is affected by which two factors?
Correct answer-Aerodynamic force / Distance from C.G. to rudder

A 100lb. weight is dropped from a height of 20ft. What is the Ep before it is dropped? Correct
answer-2,000ft/lbs

What is the KE of the same weight at the moment of impact after falling 20 feet? Correct answer-
2,000ft/lbs

In order to increase CL, high lift devices... Correct answer-Any of these answers

AOA is measured between the Correct answer-Chord line and relative wind

Vortex generators increase lift by Correct answer-adding kinetic energy to the boundary layer

An increase in air density affects the air density by Correct answer-Decreasing

Slots increase energy in the boundary layer by allowing air from below the wing to slip through the
wing during high AOA flight Correct answer-True

Fowler flaps increase a wings Correct answer-camber and surface area

The momentum change theory of lift production states that by accelerating airflow downward, lift is
created. This is explained by... Correct answer-Newton

The earth's atmosphere contains a constant amount of nitrogen, oxygen, and other gases but
increases in density with an increase in altitude Correct answer-False

The standard atmospheric values are Correct answer-- 15 degrees Celsius
- 59 degrees Fahrenheit
- 29.92"

, Which best describes now lift is created? Correct answer-Newton and Bernoulli's theories together

According to Bernoulli's principle; in a Venturi with mass flow, if dynamic pressure increases, static
pressure will? Correct answer-Decrease

Which wing exhibits the most favorable stall characteristics? Correct answer-Rectangular

What is considered "favorable stall characteristics" Correct answer-Stalling at the wing root first to
enable good slow flight control with ailerons

The CG Correct answer-Is a point where the sum of weight vectors of every party of the aircraft act

The following is a practical application of the Bernoulli's theorem Correct answer-The Venturi

At what height is experienced half the weight of the atmosphere? Correct answer-18,000 feet

What affects total lift production Correct answer-The net effect of airflow around the airfoil

Bernoulli's Principle would show Correct answer-A decrease in the speed of flow would cause
increase in the fluids static pressure

Most of the weather is contained in which layer of the atmosphere? Correct answer-Troposphere

What two things in the lift equation can you control directly to affect lift while maneuvering the
aircraft? Correct answer-Coefficient of Lift and Velocity

What best describes the turning of air around a rotating cylinder that generates up-wash, down
wash, and lift Correct answer-Magnus effect

Ozone exposure is greater in which part of the atmosphere? Correct answer-Lower stratosphere

Drag is... Correct answer-Resistance to airflow

Parasite drag is the sum of... Correct answer-Pressure drag and drag caused by skin friction

Viscosity is part of the reason air separates from the surface of the wing Correct answer-True

The boundary layer is Correct answer-The area between the surface of the wing and free stream
air

The area where laminar becomes turbulent is called? Correct answer-Transition region

Separation along an aerodynamic object occurs because Correct answer-Because of adverse
pressure gradient and the shape of the object

Ground effect has a tendency to make an airplane behave like it has a Correct answer-higher
aspect ratio

When a wing is within 1/10 of its span to the surface, its induced drag is reduced Correct answer-
by nearly half
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