Aircraft Propulsion Systems
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Aircraft Propulsion Systems

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Questions and Answers

In propulsion by action, a great ______ of air is expelled rearwards with a low increase of speed.

mass

In propulsion by reaction, the forward force is produced by expelling a ______ of gas with a certain speed.

mass

The principle of operation of a jet engine is similar to a ______ engine in that the processes such as induction, compression, ignition and exhaust are the same.

piston

The ambient air enters the engine through the ______ intake.

<p>air</p> Signup and view all the answers

The air is then compressed by a multi- stage axial ______.

<p>compressor</p> Signup and view all the answers

The combustion is achieved in an ______ chamber.

<p>annular</p> Signup and view all the answers

Gas turbine engines are divided into two main classes: ______ jet engine and Turbo prop engine.

<p>Turbo</p> Signup and view all the answers

The forward force 'F' is given by 'F' = m (V2- ______).

<p>V1</p> Signup and view all the answers

The primary aircraft controls are arranged as follows: a control ______ governs the aircraft's roll and pitch.

<p>yoke</p> Signup and view all the answers

The ______ pedals, to control yaw, which move the rudder.

<p>rudder</p> Signup and view all the answers

The throttle controls are used to control engine ______ or thrust for powered aircraft.

<p>speed</p> Signup and view all the answers

The trim tabs are small control surfaces connected to the trailing edge of a larger control surface of ______.

<p>aircraft</p> Signup and view all the answers

Trim tabs are used to control the ______ of the controls, i.e. to counteract aerodynamic forces and stabilise the aircraft in a particular desired attitude.

<p>trim</p> Signup and view all the answers

Air brakes or speed brakes are a type of flight control surface used on an aircraft to increase ______ or increase the angle of approach during landing.

<p>drag</p> Signup and view all the answers

Spoilers are designed to increase ______ while making little change to lift.

<p>drag</p> Signup and view all the answers

Spoilers reduce the ______-to-drag ratio and require a higher angle of attack to maintain lift, resulting in a higher stall speed.

<p>lift</p> Signup and view all the answers

The fuselage is the main body of the ______ to which all the other components are attached.

<p>aircraft</p> Signup and view all the answers

Early aircraft were constructed of ______ frames covered in fabric.

<p>wood</p> Signup and view all the answers

As monoplanes became popular, ______ frames improved the strength.

<p>metal</p> Signup and view all the answers

Some modern aircraft are constructed with ______ materials for major control surfaces.

<p>composite</p> Signup and view all the answers

The Boeing 787 makes possible higher ______ levels and larger windows for passenger comfort.

<p>pressurization</p> Signup and view all the answers

The cockpit is where the pilot controls the ______.

<p>aero-plane</p> Signup and view all the answers

A wing is a type of ______ with a surface that produces lift for flight or propulsion.

<p>fin</p> Signup and view all the answers

Wings have an ______ shape, a streamlined cross-sectional shape producing a useful lift to drag ratio.

<p>airfoil</p> Signup and view all the answers

During such occasions, the instruments of an aircraft play a very vital role in aiding the pilot to fly the aircraft ______.

<p>safely</p> Signup and view all the answers

The ______ indicator is an instrument used in an aircraft to display the craft's airspeed to the pilot.

<p>air speed</p> Signup and view all the answers

The static pressure is due to the pressure exerted by the ______ and the dynamic is due to the movement of the tube through the air.

<p>atmosphere</p> Signup and view all the answers

The dynamic pressure is calculated as: Dynamic = ______ – Static.

<p>Pitot</p> Signup and view all the answers

The ______ pressure remaining constant in the entire case, the variation is only in the pitot pressure due to the movement of the aircraft in air.

<p>static</p> Signup and view all the answers

An ______ is an instrument used to measure the altitude of an object above a fixed level usually the sea level.

<p>altimeter</p> Signup and view all the answers

The atmosphere has weight and this weight exerts ______.

<p>pressure</p> Signup and view all the answers

Altitude can be determined based on the measurement of ______ pressure.

<p>atmospheric</p> Signup and view all the answers

The radar signals that are reflected back towards the transmitter are the desirable ones that make radar ______.

<p>work</p> Signup and view all the answers

In aviation, aircraft are equipped with radar devices that warn of obstacles in or approaching their ______ and give accurate altitude readings.

<p>path</p> Signup and view all the answers

Primary radar uses the principle of ______ technique to determine range and bearing of an object.

<p>pulse</p> Signup and view all the answers

In secondary radar, active cooperation of the other ______ is required.

<p>object</p> Signup and view all the answers

In continuous wave radar, both the transmission and the reception take place ______.

<p>continuously</p> Signup and view all the answers

Understanding the basic functions of Radar would help cadets in better assimilation of facilities available in the ______ and their role in promoting safe flying.

<p>ATC</p> Signup and view all the answers

Study Notes

Propulsion Systems

  • Propulsion by Action: rotates a propeller in air to create aerodynamic forces and accelerate air mass, expelling a large mass of air rearwards with low speed increase.
  • Propulsion by Reaction: expels a small mass of gas with high speed, producing a forward force, as per the principle of jet propulsion (F = m(V2 - V1)).
  • Indirect Reaction Propulsion: transforms gas kinetic energy into mechanical energy, e.g., turbo shaft and turbo prop engines.

Jet Engines

  • Divided into two main classes: Turbo jet engine and Turbo prop engine.
  • Operating principle similar to piston engines, but with continuous processes instead of intermittent ones.
  • Ambient air enters the engine through air intake, gets compressed, and then combustion occurs in an annular chamber, expelling gases at high velocity to create thrust.

Aircraft Controls

  • Primary controls:
    • Control yoke (or column) governs roll and pitch by moving ailerons and elevators.
    • Rudder pedals control yaw by moving the rudder.
    • Throttle controls engine speed or thrust.
  • Secondary controls:
    • Trim tabs adjust the neutral or resting position of control surfaces to counteract aerodynamic forces.
    • Air brakes and spoilers increase drag or angle of approach during landing.
    • Flaps, leading edge slats, and variable-sweep wing.

Aircraft Design and Materials

  • Fuselage layout: comprises fire wall, wing attachment points, landing gear attachment points, stringers, bulk head/formers, and stressed skin.
  • Materials used:
    • Wood (early aircraft)
    • Metals (improved strength)
    • Composites (modern aircraft, e.g., Boeing 787)

Wings and Fuselage

  • Fuselage: main body of the aircraft, containing the cockpit, providing space for freight and passengers.
  • Wings: type of fin with an airfoil shape, producing lift for flight or propulsion through the atmosphere.

Instruments

  • Airspeed Indicator: measures airspeed by comparing static and pitot pressures, using an open-ended capsule inside an airtight case.
  • Altimeter: measures altitude above mean sea level by measuring atmospheric pressure.
  • Radar: warns of obstacles, provides accurate altitude readings, and uses pulse technique to determine range and bearing.
  • Types of Radar:
    • Primary Radar: uses pulse technique, working on echo and search light principle.
    • Secondary Radar: requires active cooperation of the other object, transmitting pulses and receiving replies.
    • Continuous Wave Radar: transmits and receives continuously, requiring a set of two aerials.

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Description

This quiz covers the basics of aircraft propulsion systems, including propulsion by action and propulsion by reaction.

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