with jet propulsion,
Air is taken in at the front, than compressed by an compressor. Fuel is added tot the air and ignites. This drives the temperature higher, making the air expand and increase the pressure. After that a turbine takes some of the energy of the flow, decreasing the temperature and pressure and converts the energy into work. the work than is used to power the compressor. The exhaust provides a thrust for the airplane.
with a propeller,
an engine drives a propeller which provides thrust for the airplane
aircraft engines are normally reciprocating engine or pistan engine, the Aircraft instruments in a reciprocating engine arecylinderpistonand so...................
im looking for the same answer
General rule: either too much heat or too much pressure. But...fails how ? on what engine and in what aircraft ? Specific questions beget specific answers
The Walter Minor is a family of four or six-cylinder inverted inline air-cooled engine used on light aircraft.
the unburned charge in the cylinders explodes instead of burning normally.
This controls the engine speed
The Boeing planes, and most modern multi-engine aircraft, can still manage to fly even if one engine stopped to function.
A glider is an aircraft that doesn't have an engine.
aircraft engines are normally reciprocating engine or pistan engine, the Aircraft instruments in a reciprocating engine arecylinderpistonand so...................
Aircraft engine manufacturers construct aircraft engines, and maintain the engines when faulty.
The aircraft maker constructs the cowlings.
An aircraft with an engine.
To "propel" the aircraft through the air.
This is a meaningless question: coefficient of lift has nothing to do with engine power or number of propeller blades - it's a function of aerofoil type (section), dynamic pressure and reference area.
engine
It depends on the size of the aircraft and the power of the engine
aircraft powerplant consist of engine, plus inlet and exhaust nozzle.