Aircraft Performance and Atmospheric Conditions

Aircraft Performance and Atmospheric Conditions

Assessment

Interactive Video

Physics, Science, Geography

9th - 12th Grade

Hard

Created by

Patricia Brown

FREE Resource

The video tutorial explains the concept of the tropopause and its impact on temperature distribution in the atmosphere. It highlights how temperature varies between the poles and the equator, affecting aircraft performance, thrust, and lift. The tutorial also discusses the role of air density in these processes and how the Flight Management System (FMS) accounts for temperature changes during flight.

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10 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the altitude of the ISA tropopause where the temperature reaches -56.5°C?

30,000 feet

50,000 feet

36,000 feet

40,000 feet

2.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

At mean sea level, what is the average temperature at the poles?

+30°C

-30°C

-40°C

0°C

3.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How does the temperature at the equatorial tropopause compare to the polar tropopause?

It is colder

It is warmer

It is the same

It fluctuates

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What happens to the temperature when an aircraft crosses the tropopause from the poles to the tropics?

It increases

It decreases

It fluctuates

It remains constant

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What is the effect on aircraft performance when flying from the tropics towards the poles?

Temperature increases, reducing performance

Temperature remains constant, no effect

Temperature fluctuates, causing instability

Temperature decreases, improving performance

6.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

How does warm air affect air density and lift?

Increases density but decreases lift

Decreases density and lift

Decreases density but increases lift

Increases density and lift

7.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What happens to engine thrust during take-off at high ambient temperatures?

Thrust increases

Thrust remains constant

Thrust fluctuates

Thrust decreases

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