15.1 fundamentals Flashcards

1
Q

what is the two classifications of energy

A
  • potential
  • kinetic
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2
Q

what is potential energy defined as

A

being energy at rest, or energy that is stored

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3
Q

what is kinetic energy defined as

A

being energy in motion

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4
Q

what are newtons three laws of motion

A

first law - law of inertia
second law - F = M x A
third law - the law of action and reaction

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5
Q

what is the measuring unit for force

A

pounds (lbs)

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6
Q

what is the thrust if the engine expressed in

A

pounds

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7
Q

what is the formula to calculate work

A

Work = force x distance

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8
Q

what is the calculation for power

A

Power = force x distance / time

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9
Q

what is acceleration defined as

A

the rate of change of velocity

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10
Q

what does speed refer to

A

how fast an object is moving

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11
Q

what does velocity describe

A

the speed of an object and the direction it is moving

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12
Q

what is the formula for kinetic energy

A

kinetic energy = 1/2 x Mass x Velocity

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13
Q

what is the brayton cycle the name given to

A

the thermodynamic cycle of a gas turbine engine that produces thrust

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14
Q

what is the variable-volume constant pressure more commonly know as

A

continuous combustion cycle

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15
Q

what are the four stage of the continuous combustion cycle

A
  1. intake (suck)
  2. compression (squeeze)
  3. expansion (bang)
  4. exhaust (blow)
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16
Q

what are the four ideal changes of state

A
  • isobaric
  • isochoric
  • isothermal
  • isentropic
17
Q

what two of the ideal change of state are of importance for aircraft gas turbine

A
  • isobaric
  • isentropic
18
Q

what does isothermal refer to

A

constant temperature

19
Q

in the brayton cycle what is the process from 2 to 3

A

isobaric heating (combustion process)

20
Q

what are the two different types of aircraft engines

A
  • piston type engine
  • gas turbine engine
21
Q

what are the four types of gas turbine engine used on aircraft

A
  • turbojet
  • turbofan
  • turboprop
  • turboshaft.
22
Q

what are the advantages of turbojet engines

A
  • relatively simple design
  • capable of very high speeds
    -takes up little space
23
Q

how much thrust does a turbofan engine produce

A

80% of the thrust from the engine

24
Q

turbo-fan engines are manufacture with either what configurations of spool(s)

A

twin spool and three spool

25
Q

what does a 3 spool engine consist of

A

an HP spool, a IP spool and a LP spool

26
Q

what are the disadvantages of turbo-fan engine

A
  • heavier than turbo jet
  • larger frontal area
  • inefficient at very high altitudes
27
Q

what is the primary difference between the turboprop and the turbojet

A

the additional turbines, a power shaft, and a reduction gear box

28
Q

what are the advantages of turboshaft engine

A
  • much higher power-to-weight ratio
  • typically, smaller than turboprop