• Aircraft Wing Structure

    In aeronautics Wing are airfoils attached to each side of the fuselage, So the design of the wing depends on many facts like lift to weight ratio, rate of climb, size, weight and which aircraft it is used,

  • AirCraft Fuselage Structure

    Fuselage is a body of an aircraft to which the wings, tail and Landing Gear units are attached. Design and size of the fuselage varies according to the function to the aircraft. The word fuselage comes from a French word “fusele” means “splindle-shape”

  • Landing Gear

    Landing gear is an undercarriage part of the flight landing system. Aircraft landing gear has wheels equipped with shock absorbers on light planes and Hydraulic or pneumatic oleo struts on larger aircraft.

Monday, December 07, 2020

Salient Features Of Scramjet Engine And Its Applications For Hypersonic Vehicles

 

Salient Features Of Scramjet Engine And Its Applications For Hypersonic Vehicles

        The scramejet uses a slightly modified Brayton Cycle to produce power, similar to that used for both the classical ramjet and turbine engine. Where Air is compressed and the  fuel injected, mixed and burned to increase the air, the combustion products are Temperature and Pressure then these combustion products are expanded.




For Turbojet engine Air is mechanically compressed by combustor using a turbine. In principle the ramjet and scramjet works the same. Where the forward motion of the vehicle compresses the air then the Fuel injected into the compressed air and burned. Results the high pressure combustion products expand through the Nozzle. Elevating the surface pressure and moving the vehicle forward.

Sunday, December 06, 2020

SCRAMJET

 

SCRAMJET


  • The wall of Ramjet will tend to fail at the higher temperature around 2500k,
  • Like Turbojets, Conventional ramjets are also limited by material problem at high Mach Number.
  • When the temperature of the air entering the combustor is too high, during which the fuel injected, it will be decomposed by the higher temperature instead been burned (Fuel will absorb rather than producing energy).
  • The engine will become a Drag producing machine instead for a Thrust producing device.
  • When the air flow is decrease by the scramjet the relative velocity and kinetic energy both decrease, during that energy required that any missing kinetic energy will reappear as internal energy.
  • When the flight Mach number exceeds about 6 led to decelerate the flow to subsonic speeds.



Advantage

  • No moving parts easies to manufacture.
  • Has less weight and simple design.
  • Does not have to carry oxygen tank.
  • High seed could be achieved easier, so cheaper access to outer space in the future.

Disadvantage

  • Scramjet cannot produce efficient thrust unless achieves high speed, around Mach 5.
  • Testing a Scramjet design requires a expensive equipments (hypersonic test chambers and launching vehicles).
  • Lack of strength.
 

 

 





Parts of Scramjet Engine

Scramjet Engine

        Scramjet is a variation of a Ramjet Engine, It is a type of Air breathing Engine where the combustion takes place in subsonic airflow, Scramjet  is supersonic throughout the entire engine , Scramjet operate more effective at extreme high speed of about Mach 5.




Parts of Scramjet Engine

  • Inlet
  • Isolator
  • Combustor
  • Nozzle



 

        The different Part of a Scramjet engine is Inlet, Isolator, Combustor and Nozzle. The scramjet engine must be integrated with the Fuselage of the aircraft, specially the air inlet and the Nozzle. Part of the forebody aircraft fuselarge makes the function of air let compressing the freestream air, and the after body acts as a nozzle expanding the gases for the combustion.


Tuesday, December 01, 2020

Salient Features of Liquid Propellant Rockets

 

Salient Features of Liquid Propellant Rockets:


                A liquid propellant propulsion system is commonly called rocket engines. It has all the hardware components and propellants necessary for its operations for producing thrust.



Liquid propellant propulsion system

Consists of one or more thrust chambers, one or more tanks to store propellants, a feed mechanism to force the propellants from the tanks into the thrust chamber, power source to furnish the energy for the feed mechanism, suitable plumbing or piping or piping to transfer the liquids,




Has a structure to transmit the thrust force, and control devices to initiate and regulate the propellant flow and thus the thrust.

In some application an engine may also include a thrust vector control system, various instrumentation and residual propellant (trapped in pipes, valves, or wetting tanks).

It does not include hardware for non-propulsive purpose, such as aerodynamic surface, guidance, or navigation equipment, or useful payload such as scientific space exploration package or missile warhead.



Friday, November 27, 2020

Ramjet Engines in Fighter Aircraft

 

Ramjet Engines in Fighter Aircraft

            Ramjet Engines is a type of Combustion Engine, comes under the category of Air breathing engine. It is the simplest of all the air breathing engines. It consists of a Diffuser, Combustion chamber and a Nozzle, and ramjets do not need any moving parts such as compressors and consequently no turbine as well.




Major Assemble of Ramjet Engines

  • Diffuser
  • Combustion Chamber
  • Nozzle




Ramjet Engines mechanism are less complicated jet engine for producing thrust in flying vehicle.

Ramjet Engines are most efficient when operated at supersonic speeds.

All the compression is occurs in the intake diffuser section producing rise in the static pressure.

When the air decelerated from a high mach number to a low subsonic mach number, it results in substantial increase in pressure and temperature so the ramjet does not need Compressor and Turbine.

 

Working

Ramjet produces power by increasing the momentum of the moving fluid by induction of energy by combustion of fuel, so the momentum of the exhaust jet greater and exceed that of the incoming air on continuous cycle.

Where the Fuel is burned the high pressure air and the mixture is then expanded to ambient static pressure through a Nozzle System.

High pressure gas expanded through the Nozzle by converting the low subsonic flow in the combustion chamber into a supersonic jet.

The combine mixture of air and fuel (supersonic jet) exhausted through the C-D Nozzle.


Working cycle of Ramjet Engines



source:NPTL

Thursday, November 26, 2020

Ramjet Engines

 

Ramjet Engines

            Ramjet Engines is a type of Combustion Engine, comes under the category of Air breathing engine. It is the simplest of all the air breathing engines. It consists of a Diffuser, Combustion chamber and a Nozzle, and ramjets do not need any moving parts such as compressors and consequently no turbine as well.


Major Assemble of Ramjet Engines

  • Diffuser
  • Combustion Chamber
  • Nozzle




Ramjet Engines mechanism are less complicated jet engine for producing thrust in flying vehicle.

Ramjet Engines are most efficient when operated at supersonic speeds.

All the compression is occurs in the intake diffuser section producing rise in the static pressure.

When the air decelerated from a high mach number to a low subsonic mach number, it results in substantial increase in pressure and temperature so the ramjet does not need Compressor and Turbine.

 

Working

Ramjet produces power by increasing the momentum of the moving fluid by induction of energy by combustion of fuel, so the momentum of the exhaust jet greater and exceed that of the incoming air on continuous cycle.

Where the Fuel is burned the high pressure air and the mixture is then expanded to ambient static pressure through a Nozzle System.

High pressure gas expanded through the Nozzle by converting the low subsonic flow in the combustion chamber into a supersonic jet.

The combine mixture of air and fuel (supersonic jet) exhausted through the C-D Nozzle.


Working cycle of Ramjet Engines



source:NPTL



Monday, November 23, 2020

Types of flow in Aerodynamic

 

Different Types of flow in Aerodynamic

    Aerodynamics is a part fluid dynamics which deals with the laws of the flow of air or other gases.



Types of flow in Aerodynamic

  • Compressible Flow
  • Viscous Flow
  • Inviscid Flow
  • Steady Flow
  • Uniform Flow
  • Rotational Flow

Compressible Flow:  Compressible flow do undergo density changes, Gases are generally compressible.

Viscous Flow: The viscosity of a fluid is a measure of its resistance to gradual deformation by shearstress or tensile stress. Viscosity is due to the friction between neighboring particles in a fluid that are moving in different velocities.

Inviscid Flow: Is the flow of an ideal fluid that is assumed to have no viscosity.

Uniform Flow: It the flow velocity is the same magnitude and direction at every point.

Rotational Flow: If the angle between the two intersecting lines of the boundary of the fluid element changes while moving in the flow.

Sunday, November 22, 2020

Turboprop Engine Components

 

What are components does Turboprop Engine have?

Turboprop Engine Components

Turboprop is one among the type of Turbine Engine which is used to drive the propeller of the aircraft.

Major assemblies of a Turboprop Engine



  • Intake
  • Propeller
  • Gear Box
  • Compressor
  • Fuel Injector
  • Combustion chamber
  • Turbine
  • Nozzle 


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Saturday, November 21, 2020

Types of Jet Engines

 

 

What are the Types of Jet Engines used in Aircraft?


Turbofan Engine



Turboprop Engine



Turbojet Engine



Turboshaft Engine



Ramjet Engine



Scramjet Engine


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Friday, November 20, 2020

Helicopter fuselages components

 

What are components does any Helicopter fuselages have?



Major assemblies of a Single-Rotor Helicopter

  • CABIN
  • COCKPIT
  • COCKPIT DOOR
  • PASSENGER DOOR
  • INTEGRAL FUEL TANK
  • BAGGAGE COMPARTMENT
  • TAIL CONE
  • HORIZONTAL STABILIZER
  • VERTICAL STABILIZER
  • BATTERY AND ELECTRICAL             COMPARTMENT
  • ENGINE COMPARTMENT
  • TRANSMISSION COMPARTMENT
  • FLIGHT CONTROL ENCLOSURE
  • ELECTRONIC COMPORTMENT

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    Sunday, September 13, 2020

    UAVs Unmanned Aerial Vehicles

     

    UAVs Unmanned Aerial Vehicles

                    After the Wright brothers worked so hard to put humans in the air by flying machines, now a day’s some aerospace engineers are working hard to take out of the flying machine. UAVs Unmanned Aerial Vehicles are the Airplanes that have no humans on board which are operated and flown remotely by pilots.




    Israel is the first nation to use UAVs in the combat situation arguing that loss of relative inexpensive UAVs was better than the loss of a pilot and a multi-million dollar airplane.

    UAVs are mainly used to carry sensors, target designated and electronic transmitters

     Designed to destroy enemy’s target, UAVs are more effective fly at greater range and endurance.

    Range – Is the maximum distance an aircraft can fly between takeoff and landing.

    Endurance – Is the maximum length of time that an aircraft can spend in cruising flight (level flight).




    Monday, August 31, 2020

    Aircraft Powerplant Outer Structures

     Aircraft Powerplant Outer Structures

                   Aircraft powerplants produces the source of thrust to move the aircraft through the air, at the same time they are also the source of vibration, heat and drag forces. Powerplant Structures includes both the propeller and Engine work in combination to produce thrust. Engine provides the source of power to rotate the propeller.  Propeller is mounted at the front of the engine converts the rotatory force into Thrust in the engine.




    Powerplant Outer Structures components

    Nacelles

    Nacelles encloses the engine provide the streamline flow (uniform flow) of air over the outer surface of the engine to improve the aerodynamics of the aircraft. Protect the engine and its components during flight. Allow the proper flow air to engine for cooling and combustion.


    Nacelles

       

    Fire walls

    Firewalls are normally located near to the engine compartment. Engine, Auxiliary power units, combustion chamber and turbine produces tremendous amount of heat which affect other aircraft component and it functionality, to protect other aircraft component from this heat effect sections of the turbine engine must be isolated from the remainder of the aircraft by means of firewalls. Firewall is used to protect the nacelle strut and systems from the exposure.

    Fire walls


    Engine Mount

    Engine mount is frame structures that support the engine and connect it to the fuselage. Which are designed to distribute the weight of the engine and distribute torque and vibration generate from the engine.


    Engine Mount


    Cowlings and Fairings

    Cowlings and Fairings both are similar, which are removable covering for covering the portions of the airplane (Engine, Mounts and other engine components). Design to provide uniform flow of air over the engine surface improve the aerodynamics of the aircraft.

    Cowlings and Fairings