Module 5 Concepts Flashcards

1
Q

What type of wave is sound?

A

Longitudinal, pressure wave

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2
Q

What assumptions are made for the speed of sound in air?

A
  • Ideal gas

- Adiabatic process

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3
Q

What is the speed of sound a function of?

A

Temperature, and temperature only!

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4
Q

What is a Mach number?

A

A dimensionless quantity which is the ratio of the speed of a flow to the local speed of sound

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5
Q

What are the three different states that air particles can be in when flowing around an object? What is their mach number?

A

Subsonic if M < 1
Sonic M = 1
Supersonic M > 1

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6
Q

What different states can an aircraft be in with respect to mach?

A

Subsonic if Mfs < Mcrit
Transonic if Mcrit < M < 1.2
Supersonic if Mfs > 1.2

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7
Q

What is the free-stream Mach number?

A

the ratio of free stream airspeed of an aircraft to the free stream speed of sound

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8
Q

What is the local mach number?

A

Ratio to of particles at a location around the aircraft to the local speed of sound

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9
Q

What is the Critical mach number>?

A

The free-stream mach number when a local mach number has reached 1. Marks when the first local airflow becomes sonic.

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10
Q

How will increasing temperature when all other factors are constant affect affect the Mach number?

A

Mach will decrease

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11
Q

When descending at a constant CAS what will happen to Mach number under ISA?

A

Mach number decreases
due to:
-LSS increasing
-TAS decreasing

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12
Q

What happens to CAS if you climb at constant Mach through an isothermal layer?

A

LSS and TAS do not change

CAS will decrease due to reduction in density

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13
Q

What will happen to displayed Mach number if the pitot port becomes blocked during a climb?

A

Machmeter will over read

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14
Q

What happens to TAS when climbing at a constant Mach?

A

Decreasing (proportionally)

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15
Q

If both ALT and TAS are constant but Mach increases, what is happening?

A

Temperature is decreasing

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16
Q

What is happening if IAS is constant but Mach is decreasing?

A

-Descent at constant IAS