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Thrust

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Turbofan has the larger bypass ratio for more efficient powerplant. * * Title: Thrust Author: Art Smith Last modified by: Art Smith Created Date: 2/7/2002 8:11:30 AM – PowerPoint PPT presentation

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Title: Thrust


1
Thrust
  • Lecture 8
  • Chapter 4

2
Thrust
  • Thrust is the force that must be generated in
    order to overcome the natural resistance of drag.
  • Because drag is the force opposite to the flight
    path, thrust must be in the direction of flight.

3
Thrust
  • If thrust is increased greater than drag, the
    speed would increase.
  • Thrust and drag are equal in straight and level,
    unaccelerated flight.
  • The thrusting force must equal the retarding
    forces in order to maintain a steady speed.

4
Newtons three laws
  • 1. A body in motion will remain in motion in
    constant speed and direction until acted upon an
    outside force A body at rest will remain at
    rest.
  • 2. Force equals mass times acceleration.
  • 3. For every action there is an equal and
    opposite reaction.

5
Principles of Propulsion
  • Newtons second law
  • A force exerted on an object of so much mass
    would accelerate it proportional to the amount of
    force.
  • F m x a
  • Force mass times acceleration
  • Acceleration is a rate of change of velocity or
    change of velocity over time.

6
Force Velocity
  • If a body were initially at rest, a force would
    give it some velocity over a period of time
    causing acceleration.
  • Air has mass, a force applied to,would accelerate
    and increase the velocity.

7
Propeller
  • A propeller is wide in diameter takes in a
    relatively large mass of air per second.
  • A reasonable amount of thrust can be created with
    a small change in velocity across the propeller
    plane a high degree of efficiency is maintained.

8
Jet Engines
  • Jet engines have a relatively small diameter
    accommodate a smaller amount of air.
  • In order to produce significant thrust, they must
    accelerate this small mass to a much larger
    velocity.

9
RAMJET
  • Ramjet-simplest form a nozzle shaped device in
    which the air is compressed by the ram effect of
    moving through the air.
  • Fuel is injected ignited the expanded gas
    exhausts at high velocity.
  • PRO simple, handle high temps high speed
  • CON must be in motion at high speed to be started

10
PULSEJET
  • Pulsejet variation of ramjet this engine has a
    shutter-like check valve is installed in the air
    inlet that works in sync. With the pulse
    injection of fuel.
  • The fuel is ignited expansion forces the check
    valve shut a burst of gas out of the exhaust.
  • Ram air then force the check valve open as the
    internal pressure drops cycle repeated.

11
PULSEJET
  • Pulsejet required a forward speed in order to
    start operation.
  • German V-1 buzz bombs of WWII
  • Usually launched by booster rockets
  • Neither the ramjet nor the pulsejet are used much
    in conventional aircraft propulsion.

12
TURBOJETS
  • Turbojets were developed in 1930s by Sir Frank
    Whittle of England.
  • Hans von Ohain of Germany was also working on a
    turbojet.
  • The Messerschmitt Me-262, the first jet-powered
    aircraft.
  • The Bell P-59, the first American jet aircraft

13
Commercial Transport
  • The de Havilland Comet was the first commercial
    jet aircraft, introduced in 1949.
  • Then came Boeing 707 and DC 3.

14
Axial-Flow
  • Incoming air is compressed by the compressor
    forced into the burner section
  • Fuel is injected ignited
  • The burning gases rapidly expand force out
    through the exhaust
  • Then it passes through the turbine, giving
    rotation motion.
  • Unused exhaust gas is expanded pressure drops
  • Acceleration of this mass of air is a thrusting
    force against the engine

15
Pure Jet
  • In a Pure Jet all of the air flows through the
    combustion section gets accelerated to high
    velocity.
  • Due to inefficiency the turbofan was designed to
    increase efficiency but retain most of the
    high-thrust ability of the turbojet.

16
Turbofan
  • In the turbofan the bypass air from the fan
    provides the increased efficiency.
  • It also derives part of its thrust from the jet
    section, accelerates the air to a higher degree
    obtains a siginificant amount of thrust.
  • Turbofan has the larger bypass ratio for more
    efficient powerplant.
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