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  • Hello and welcome to this video tutorial on the basics of

  • Aerodynamics.In tutorial, we will discuss what makes

  • an airplane fly, and we'll learn some important terms and concepts

  • along the way.But first

  • let's learn about the Bernoulli's principal. Daniel Bernoulli,

  • who is a Swiss mathematician, expanded

  • on Newton's ideas and discovered the motion of fluids.

  • He described in his 1738 publication,

  • "Hydrodynamica," the basic principles

  • of airflow pressure differential. The principle

  • simply states that as the velocity of a fluid, such as air,

  • increases its pressure decreases.

  • let's take a look at the diagram

  • to understand this concept a little better. As the air

  • or fluids in general travel through the tighter passage of the tube,

  • the velocity increases since fluids

  • travel at a faster speed to reach

  • the end of the curve.What's interesting,

  • when he measured the pressure, Bernoulli discovered that every time the

  • velocity increased

  • or decreased the pressure would have the opposite effect

  • In this slide

  • will define a very important force that will help us

  • understand the future concepts.That force is the "Relative

  • Wind."The relative Wind is simply the airflow that is parallel

  • and opposite to the flight path the airplane. An airfoil

  • is any surface, such as a wing, that provides

  • aerodynamic force when it interacts with a moving stream

  • of air.When given a flight path

  • and an opposite relative wind

  • it' s important to remember

  • that the airflow over the surface of the wing

  • will have a higher velocity than the airflow

  • under the wing. it's also important to note

  • that the circulation on the airstream about the

  • airflow is an important factor in the generation

  • of lift. The Camber

  • it is

  • the characteristic curve of the airfoil's upper

  • and lower surfaces. The Chord line

  • is an imaginary straight-line

  • drawn through the airfoil and the direction of

  • the relative wind. The chord line

  • is a very important determinant of what's called

  • the "Angle of Attack."The angle of attack

  • is simply the angle between the Chord line

  • and airflow at the direction

  • of the relative wind. In this slide

  • we will learn that as the angle of attack increases

  • the lift also increases.

  • Please note that the lift acts perpendicular

  • to the relative wind regardless of the angle

  • of attack. According to Bernoulli's Theorem,

  • the increased speed of the air on top of an airfoil

  • produces a pressure drop. This lowered

  • pressure is one component of a total

  • lift. However,

  • when the angle of attack is increased

  • beyond the maximum allowed the lift

  • is decreased; this causes

  • what's called a "Stall." As we mentioned earlier,

  • a stall is the result of

  • a critical angle attack. It is also caused

  • by the disruption on the airflow

  • from the upper surface of the wing

  • or airfoil. The airflow then separates

  • at what's called the "Trailing Edge."

  • The airflow progresses forward until the wing

  • is fully stalled

  • Therefore, a stall is a rapid decrease

  • of lift caused by separation of

  • airflow. In this slide,

  • we will learn about the four very important forces

  • of flight. The challenge

  • to understand what makes an airplane fly

  • starts with learning the four forces of flight.

  • During a flight, the four forces

  • acting on the airplane are : Lift,

  • Weight, Thrust, and Drag

  • Lift as we discussed earlier is created

  • by the effect of airflow over and under

  • the wing. The weight of the airplane

  • that is the force caused by gravity.

  • The Thrust: That is the force that propels

  • the airplane. And finally,

  • the drag, which is the force that limits

  • the speed of the aircraft.

  • By now we have established that lift is the key

  • aerodynamic force. Please remember

  • that when

  • weight and lift are equal

  • an airplane is said to be in a state of

  • equilibrium, and that means

  • Lift = Weight also,

  • when vertical and horizontal forces are applied

  • as shown on the left of the slide, the resulting force

  • acts in a diagonal direction

  • therefore the resultant of two

  • opposing forces which are equal in magnitude

  • is zero. I hope you enjoyed the tutorial

  • and thank you for watching :)

Hello and welcome to this video tutorial on the basics of

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航空力学の基礎 (The Basics of Aerodynamics)

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    Nathan に公開 2021 年 01 月 14 日
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