Evolution of Flight
Aircraft Control Surfaces
Forces of Flight
Weight & Balancce
Just For Fun
100

What two brothers are credited with making the first successful powered, controlled flight in 1903?

Wright Brothers

100

Which control surface controls roll?

Ailerons

100

What force acts upward on an aircraft?

Lift

100

What is the fixed reference point used for weight-and-balance calculations called?

Datum

100

What is my room number?

C102

200

What inspired the Montgolfier brothers to develop lighter-than-air flight?

Rising smoke

200

Which control surface controls the nose moving up and down?

Elevator

200

What force acts opposite the direction of flight?

Drag

200

What is the distance from the datum to where an item's weight acts called?

Arm, or moment arm

200

How many computers are in this room? 

You may not count.

26

300

Who flew the first nonstop flight across the Atlantic Ocean in 1927?

Charles Lindbergh

300

Which control surface controls the nose moving left and right?

Rudder

300

If thrust is 8,000 N and drag is 5,000 N, what is the resultant force?

3,000 N forward

300

What is the formula for calculating moment?

Moment = Weight × Arm

300

Name all of the admins.

Besli, Hasni, Topsakal, Mercan

400

What was the name of the aircraft that made the Wright brothers’ famous 1903 flight?

The Wright Flyer

400

What are the three basic rotational movements of an airplane?

Roll, pitch, and yaw

400

If lift is greater than weight, what happens to the aircraft?

It accelerates upward

400

Calculate the moment: 100 lb of weight located 5 ft from the datum.

500 ft-lb

400

What is the school's address?

13738 Old Richmond Rd, Sugar Land, TX 77498

500

What pilot flew faster than the speed of sound in 1947, reaching approximately Mach 1.06?

Captain Chuck Yeager

500

What control surface is located on the wings, moves downward together, and increases both lift and drag?

Flaps

500

An aircraft has 6,000 N of thrust and 6,000 N of drag. What is the resultant force, and what happens to its motion?

The resultant force is 0 N. The aircraft does not accelerate or decelerate and can continue at a constant velocity

500

An aircraft has a total weight of 2,000 lb and a total moment of 100,000 in-lb. What is its center of gravity?

CG = Total Moment ÷ Total Weight 

= 100,000 ÷ 2,000 = 50 inches from the datum

500

Spell Ms. Feride's last name.

(Turkish people are exempt from this question)

Tiryakioglu