combution chamber in jet engine .
air and fuel mixer burned in combution chamber by using igniter, then burent fuel mixer having with high pressure and high temperature . stagnation enthalpy temperature increases due to combution fuel -air mixture.
thrust :thrust is forward force , push the engine : thrust is reducing then velocity increases., of flight .
bhanu chander, p.b college of engineering .aeronautical engineering -9092149838
the hottest point of the jet engine is the combustion chamber
Air. Air and heat are the basis of the jet. The reason for this is that in the combustion chamber compressed air is ignited. The air flow pushes this reaction out the back of the engine and this= thrust.
Oxygen is the gas needed for a jet engine to burn its fuel. It combines with the fuel in the combustion chamber to generate the necessary energy for thrust.
Volcanic ash effects jet engines by clogging-up the engine. The plane travels at such a speed even minute particles like volcanic ash can eventually fill-up the combustion chamber and since there is no moving parts in a jet engine it can't get out of the chamber. The massive heat in the chamber turns the volcanic ash to glass because its 80% silica which eventually stops everything in the engine (Basically).
The temperature inside the combustion chamber of a jet engine can reach up to 2,000 to 3,000 degrees Fahrenheit (1,100 to 1,650 degrees Celsius) due to the combustion of fuel with compressed air. This high temperature is necessary to achieve efficient fuel combustion and generate the thrust needed for the aircraft to operate.
In a jet engine, fuel is injected into the high-pressure air that has been compressed by the engine's compressor. This fuel is typically aviation kerosene, such as Jet A or Jet A-1. Once injected, the fuel mixes with the compressed air and is ignited in the combustion chamber, producing high-temperature, high-pressure exhaust gases that propel the engine and generate thrust.
Frank Whittle, a British pilot, designed the first turbo jet engine in 1930. The first Whittle engine successfully flew in April, 1937. This engine featured a multistage compressor, and a combustion chamber, a single stage turbine and a nozzle. In 1900 there were no jet around to carry a bunch a people.
There are a few different jet engines, but it basically needs bleed air and fuel. Air enters the engine where it is compressed and mixed with fuel. Next, the air/fuel is heated in a combustion chamber, then it is unleashed through the turbine as thrust.
jet engine
Frank Whittle was the invetor of the jet engine.
You can but a mini jet engine on ebay.
A jet engine compressor works by drawing in ambient air and compressing it to increase its pressure and temperature. This is achieved through a series of rotating blades and stationary vanes that sequentially compress the air as it moves through the engine. The compressed air is then mixed with fuel and ignited in the combustion chamber, producing high-velocity exhaust gases that propel the aircraft forward. The efficiency of the compressor is crucial for the overall performance and thrust of the jet engine.