The Physics of Flight Flashcards

Newton's Laws of Motion

1
Q

Which one of Newton’s Laws of motion is this?
“An object at rest will remain at rest and an object in motion will remain in motion.”

A

Newton’s First Law of Motion aka Law of Inertia

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2
Q

Out of the 4 types of friction, which one is this?
“This friction is the result of when the surface of one object slides along the surface of another object.”

A

Sliding, or Kinetic Friction

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3
Q

Out of the 4 types of friction, which one is this?
“This friction is the result of the resistance on an object when it is moved through either air (gas) or water (liquid).”

A

Fluid Friction

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4
Q

Out of the 4 types of friction, which one is this?
“Similar to sliding friction except this friction occurs when an object rolls across a surface.”

A

Rolling Friction

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5
Q

Out of the 4 types of friction, which one is this?
“Keeps an object at rest when that object is acted upon by an external force.”

A

Static Friction

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6
Q

Which one of Newton’s Laws of motion is this?
“When a body is acted upon by a constant force its resulting acceleration is inversely proportional to the mass of the body and directly proportional to the applied force.”

A

Newton’s Second Law of Motion

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7
Q

Which one of Newton’s Laws of motion is this?
“for every action, there is an equal and opposite reaction.”

A

Newton’s Third Law of Motion

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8
Q

Definition: “A particle attracts every other particle in the universe with a force that is directly proportional to the product of their masses and inversely proportional to the square of the distance between them.”

A

Newton’s Law of Universal Gravitation

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9
Q

Definition: “Points of faster fluid speed will experience less pressure than points of slower fluid speed.”

A

Daniel Bernoulli’s Principle

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10
Q

Definition: “Provided by the aircrafts manufacturer along with a weight limit, which is specific to each aircraft.”

A

Empty weight center of gravity (EWCG)

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11
Q

Definition: “Total weight aircraft was built. Includes systems components required for the aircraft to operate. Does not include, baggage, passengers, or either usable or unusable fuel or fluids.”

A

Manufacturer’s empty weight (MEW)

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12
Q

Definition: “MEW plus weight of the crew, fluids, unusable fuel, and equipment. Does not include baggage, passengers, or usable fuel.”

A

Operating Empty Weight (OEW)

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13
Q

Definition: “the total aircraft weight at any moment during the flight or ground operation. This weight will decrease during a flight due to fuel and oil consumption.”

A

All-up Weight or Aircraft Gross Weight

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14
Q

Definition: “the maximum weight limit at which an aircraft is certified to land safely.”

A

Maximum Landing Weight (MLW)

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15
Q

Definition: “the maximum weight of an aircraft allowed with all non-fuel elements onboard, but before any fuel is loaded.”

A

Maximum Zero Fuel Weight (MZFW)

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16
Q

Definition: “the maximum weight an aircraft is certified to take off at, determined by the manufacturer, due to structural or other limits.”

A

Maximum Takeoff Weight (MTOW)

17
Q

Definition: “the highest weight an aircraft can have while on the ground, including fuel for taxi and run-up.”

A

Maximum Ramp Weight (MRW)

18
Q

Definition: “defines an aircraft’s safe operating boundaries concerning factors like speed, altitude, and angle of attack.”

A

Flight Envelope

19
Q

Definition: “the angle at which the chord of an aircraft’s wing meets the relative wind.”

A

Angle of Attack

20
Q

Definition: “the downward deflection of air caused by the aerodynamic action of a wing or rotor blade.”

21
Q

Definition: “the type of aerodynamic drag caused by any aircraft surface that disturbs or interferes with the smooth airflow around the airplane, encompassing all drag except for lift-induced drag.”

A

Parasite Drag

22
Q

Definition: “produced mainly by the shape of the aircraft.”

A

Profile Drag

23
Q

Definition: “Air flowing rapidly across the top of a wing meets air flowing more slowly underneath. This drag increases when lift, airspeed, and AOA increase.”

A

Induced Drag

24
Q

Air weighs approximately how many pounds per square inch (psi)?

25
Q

What two atmosphere factors reduce an aircraft’s capability for power, thrust, and lift?

A

Humidity and low air density levels

26
Q

What are the 4 atmospheric factors that affect an aircraft’s performance?

A

Pressure, Altitude, temperature, and humidity

27
Q

The pressure altimeter is automatically calculated at how many inches of mercury (Hg)?

28
Q

What are the two types of aircraft structures?

A

1.) Truss
2.) Monocoque

29
Q

What type of aircraft structure is this?

  • Consists of welded steel-tubing longerons separated by diagonal members to endure the loads placed on aircraft
A

Truss Structure

30
Q

What type of aircraft structure is this?

  • Consists of a thin sheet-aluminum alloy curved to fit the shell of the fuselage. The metal skin is designed to withstand the stress of loads and minimize the total weight of the aircraft.
A

Monocoque Structure