Aerospace Knowledge Quiz

Aerospace Knowledge Quiz

University

•

60 Qs

quiz-placeholder

Similar activities

Semester 2-IPC Exam (M)

Semester 2-IPC Exam (M)

KG - University

•

61 Qs

Patalasanlahi Review IV (Physics and Chemistry)

Patalasanlahi Review IV (Physics and Chemistry)

7th Grade - Professional Development

•

63 Qs

Aircraft Weighing Midterm without ASA questions

Aircraft Weighing Midterm without ASA questions

University

•

63 Qs

Personality development MCQs

Personality development MCQs

University

•

62 Qs

Properties of Waves

Properties of Waves

KG - University

•

60 Qs

6/5/2020

6/5/2020

11th Grade - University

•

63 Qs

Prof-Ed Review Masterclass

Prof-Ed Review Masterclass

University

•

63 Qs

Unit10: Simple Harmonic Motion/Geo. and Phys. Optics F exam rev.

Unit10: Simple Harmonic Motion/Geo. and Phys. Optics F exam rev.

12th Grade - University

•

60 Qs

Aerospace Knowledge Quiz

Aerospace Knowledge Quiz

Assessment

Quiz

•

Physics

•

University

•

Practice Problem

•

Medium

Created by

Guitar (TheLifeIsHard)

Used 1+ times

FREE Resource

AI

Enhance your content in a minute

Add similar questions
Adjust reading levels
Convert to real-world scenario
Translate activity
More...

60 questions

Show all answers

1.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

What mainly determines the speed of sound in the atmosphere?

Air density

Air temperature

Altitude

Humidity

2.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

At a constant IAS, Mach number will:

Increase with altitude

Decrease with altitude

Stay the same at all altitudes

Depend only on humidity

3.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Stall speed increases when:

Air density increases at low altitude

Altitude increases due to lower density

Temperature increases significantly

Thrust-to-weight ratio is higher

4.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

The speed ranges are usually divided into:

Transonic → Hypersonic → Subsonic

Supersonic → Transonic → Subsonic

Subsonic → Transonic → Supersonic

Subsonic → Supersonic → Hypersonic

5.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

When an aircraft reaches its Critical Mach number:

Shock waves begin to form on the wing

Stall occurs immediately

The center of gravity shifts aft suddenly

Lift increases abruptly

6.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Mach tuck can be described as:

Nose-up pitching moment at low AoA

Nose-down pitching moment due to aft CP shift

Rolling moment caused by asymmetric stall

Yaw instability at high Mach

7.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Conventional empennage configuration refers to:

Elevator mounted on fin

Horizontal tailplane behind main wing

Tailplane in front of main wing

V-tail arrangement

Access all questions and much more by creating a free account

Create resources

Host any resource

Get auto-graded reports

Google

Continue with Google

Email

Continue with Email

Classlink

Continue with Classlink

Clever

Continue with Clever

or continue with

Microsoft

Microsoft

Apple

Apple

Others

Others

Already have an account?