raise the elevatord
lower the elevators
dip down
longitudinal axis
at trailing edge of the wings
the left aileron goes up and the right aileron goes down
yaw has to do with turning the airplanes nose right or left
turn the rudder right
turn the rudder left
at the trailing edge of the vertical stabilizers
he or she must do a combination of yawing and rolling
yaw right roll right
yaw left roll left
they are based on the principle that when possible air pressure tries to equilaze. And they are based on the principle that if is a force that is directed in one direction there will be an equal force directed in the opposite direction
jet engines propellers and rocket launchers
true
air is taken in = the engine sucks in air in the front with a fan
the air is compressed = a set of blades attached to a shaft rotates. this compresses the air thus raising the pressure of the air
the compressed air is fueld with gas and ignited = the compressed air is then is sprayed with fuel and an electric spark lights the mixture
the gas mixture expands quickly as it expands = as the gas mixture burns it expands very expands furthur. this raises the pressure in the combustion chamber even more
the gases gush through the jet nozzle toward the ground with a tremendous amount of force
the rocket lifts off the launch pad in the oposite direction as the escaping gases. the force of the escaping gases are enough to launch the rocket
liqued oxidizer and liquid fuel
they burn this fuel and oxidizer
fuel is mixed with oxegen
the fuel oxegen is ignited in a combustion chamber. this produces large amounts of heat and gases
the hot gases become compressed as they fill the combustion chamber. The pressure inside the combustion chamber is very high compared to the surrounding air pressure
the compressed gases are allowed to escape through a jet nozzle .
the gases escape through nozzles = the air that is being pressured tries to equalize with the air around the engine. they are able to escape through tiny holes called nozzles
the escaping vapours provide thrust = the gases exit the engine with great force which provides thrust moving the rocket forward