Yes. See link below.
the hottest point of the jet engine is the combustion chamber
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.
A jet engine typically consists of several key components, generally categorized into four main sections: the intake, compressor, combustion chamber, and turbine. Within these sections, there are numerous individual parts, including fan blades, compressor stages, fuel injectors, and nozzle assemblies. The exact number of parts can vary significantly depending on the engine design and model, but a modern commercial jet engine may have thousands of individual components.
The Germans invented the first operational jet engine during WW2.
The thrust of a Jet engine is calculated through the formula: F=(m_air+m_fuel)*v_e - m_air*v Where m_air is the mass flow rate of air entering into the engine m_fuel is the mass flow rate of fuel entering the combustion chamber v_e is the exit velocity of the exhaust gases (where v_e needs to be subsonic) v is the velocity of air entering the engine As you can see the thrust is reduced by the term m_air*v which physically has the significance of a drag at the intake of the engine. That's why rocket engine give usually a better thrust. Since they carry the oxidizer on-board that term doesn't exist for a rocket engine. I will let you think about the parameters you can play with to design an engine with as highest thrust as possible for a given (fixed fuel consumption). hint:v_e is influenced by things like combustion temperature, combustion pressure etc... Hope this helps!
Airplane is a device powered either by a piston engine and prop or by a jet engine.
A jet engine powered car works by using a gas turbine engine to generate thrust, which propels the vehicle forward. The engine burns fuel to create hot gases that are expelled at high speeds, creating the necessary force to move the car. The advantages of a jet engine powered car over traditional combustion engine vehicles include higher power-to-weight ratio, faster acceleration, smoother operation, and potentially lower emissions. Additionally, jet engines are more efficient at high speeds, making them ideal for high-performance vehicles.
They are either powered by a turbine engine like a jet engine or a piston engine.
the hottest point of the jet engine is the combustion chamber
can't be sure, but i would definably say jet engine, or else they would use combustion engines with propellers on every airplane
The combustion of the jet fuel in the engine of a jet aircraft propells the craft forward when it exits the nozzles of the jet engine(s) at high speed.
A hydrogen combustion engine is like the engine in your car. Hydrogen and oxygen enter a combustion chamber, ignite, and form a ball of hot vapour (steam) which moves a piston that rotates a crankshaft. Alternately a hydrogen combustion engine could be a rocket or jet engine where the burning fuel exhausts the combustion chamber as vapour (steam again) and impacts a forward motion to the engine by the mass discharge. A fuel hydrogen cell is more like a battery. Hydrogen and oxygen react in a catalyst matrix that allows the process to continue at a fixed rate. Like most chemical reactions this involves the movement of electrons to create positive and negative reactant ions. The flow of electrons is conducted to an electrical system as power. Water is still the byproduct.
A steam engine, a stirling engine, a combustion engine, a jet engine, a rocket engine.
An aeroplane's engine sucks air. Combustion takes place due to jet fuel. The force of the combustion propels the aircraft.
First jet fuel is ignited by an electrical pulse.The flowing air supports the combustion.
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.
The hot section is the combustion area of the engine located in the aft section before augmentation.