Lift

Lift

University

7 Qs

quiz-placeholder

Similar activities

Transonic flow over wing CO5

Transonic flow over wing CO5

University

9 Qs

TUTORIAL 3c - CHAIN DRIVE

TUTORIAL 3c - CHAIN DRIVE

University

10 Qs

Well Surveying

Well Surveying

University

10 Qs

VEX Parts Quiz

VEX Parts Quiz

8th Grade - University

9 Qs

curves

curves

University

5 Qs

Communications 4 - Quiz 2

Communications 4 - Quiz 2

University

12 Qs

Airport Design Considerations Quiz

Airport Design Considerations Quiz

University

10 Qs

Kinematics of Robots

Kinematics of Robots

University

10 Qs

Lift

Lift

Assessment

Quiz

Engineering

University

Medium

Created by

Ted Sian Lee

Used 2+ times

FREE Resource

7 questions

Show all answers

1.

MULTIPLE SELECT QUESTION

1 min • 1 pt

[Multiple correct answers] A ping pong ball is rotating in a clockwise direction while translating from right to left. Choose the correct statements.

The velocity is reinforced on the top of the ball and reduced at the bottom side.

The velocity is reinforced on the bottom side of the ball and reduced at the top.

The stagnation points move towards the bottom of the ball.

The stagnation points move towards the top of the ball.

2.

FILL IN THE BLANK QUESTION

30 sec • 1 pt

The lift due to the rotation of a body is known as the __________ effect?

3.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Media Image

Which of the following statements correctly describes the lift coefficient equation shown?

The equation is true for airfoil with finite length and large angle of attack.

The equation is true for airfoil with finite length and small angle of attack.

The equation is true for airfoil with infinite length and small angle of attack.

The equation is true for airfoil with infinite length and large angle of attack.

4.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

Planform area of the wing equals to the

Wing span × chord length

Wing span × wing thickness

Chord length × wing thickness

Cross-sectional area of the wing

5.

MULTIPLE CHOICE QUESTION

30 sec • 1 pt

What does airfoil stall mean?

The airfoil experiences a sudden increase in acceleration

The airfoil experiences a sudden decrease in acceleration

The airfoil experiences a sudden increase in lift

The airfoil experiences a sudden loss of lift

6.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

The following statements are correct except

Wing tip vortices increases the effective angle.

Wing tip vortices creates a downwash.

Wing tip vortices leads to an induced drag.

Wing tip vortices results in a smaller effective lift.

7.

MULTIPLE CHOICE QUESTION

45 sec • 1 pt

Media Image

Based on the figure shown, which type of wing design is preferable?

Smaller wing span, larger chord length

Smaller wing span, smaller chord length

Larger wing span, smaller chord length

Larger wing span, larger chord length