Since an object orbiting the earth is falling as it orbits, does it gradually ge…

Since an object orbiting the earth is falling as it orbits, does it gradually get closer to the earth? Would it eventually reenter the earth’s atmosphere and fall to the ground?-MG

If the orbiting object doesn’t interact with anything but the earth, then the answer is: no, it will continue to orbit forever. That’s because, although it is always falling and accelerating toward the earth, its sideways velocity continues to make it miss the earth. It just keeps on missing forever. Moreover, its total energy remains constant—the sum of its kinetic and gravitational potential energies. But if something removes some of its energy, it will gradually shift closer and closer to the earth and will reenter the atmosphere. That reentry occurs for low-lying satellites because they interact with the diffuse atoms in the extreme upper atmosphere. These satellites gradually lose energy and eventually come down in a blaze of frictionally heated material.

How is it that gas moving very rapidly is unable to “communicate” with gas or …

How is it that gas moving very rapidly is unable to “communicate” with gas or surfaces in front of it?

When gas is moving slowly through a channel, it can respond to obstacles by flowing around them. For example, when the gas encounters a constriction in the channel, it speeds up to flow quickly through the narrowing and its pressure drops. But when the gas is moving very fast through the channel, it has trouble avoiding obstacles and behaves differently at a constriction. Instead of speeding up to flow smoothly through the narrowing, the gas collides with the walls of the constriction and is pressure rises. It just wasn’t able to “sense” the presence of the constriction before it actually hit the constriction. When gas moves faster than the speed of sound in that gas, it can’t anticipate changes in its environment and it doesn’t follow Bernoulli’s equation. That’s why the nozzle of a rocket flares outward to handle the supersonic gas that emerges from the nozzle’s throat. That high-speed gas experiences a pressure drop as it spreads out into the broad portion of the nozzle. The gas’s density drops and its pressure goes down.

How does the use of sticks and fins stabilize rockets?

How does the use of sticks and fins stabilize rockets?

Sticks and fins both shift a rocket’s center of aerodynamic pressure (center of drag) toward the tail of the rocket and behind the rocket’s center of mass. As a result, the tail of the rocket normally remains at the rear during flight. The passing air twists the tail of the rocket until it’s at the rear of the moving object.

How does a rocket engine work?

How does a rocket engine work?

A rocket engine works by ejecting stored material. It pushes on this material to make the material accelerate and the material pushes back on the engine. If the force that the ejected material exerts on the engine is upward and greater than the rocket’s weight, the rocket will accelerate upward.

Most rocket engines are chemical engines. They combine stored chemical fuels to produce hot, high-pressure gas. This gas is allowed to expand out of a narrow orifice—the throat of the engine’s exhaust nozzle. Gases always accelerate toward lower pressure, so the high-pressure gas moves faster and faster as it rushes out of the nozzle. It reaches sonic velocity (the speed of sound) in the nozzle’s throat and continues to move faster and faster as it flows out of the nozzle’s widening bell. By the time the gas leave the engine completely, it’s traveling several thousand meters per second. A liquid fuel rocket has an exhaust velocity of about 4,500 meters per second or about 3 miles per second. Accelerating the gas to this enormous speed takes a huge force—the engine pushes down hard on the gas. The gas pushes back and propels the rocket upward.

How can the total momentum still be zero when two objects are moving rapidly awa…

How can the total momentum still be zero when two objects are moving rapidly away from each other?

Momentum is a vector quantity, meaning that it has both an amount (a magnitude) and a direction. When two objects are moving rapidly away from one another, they each have momentums but those momentums are in opposite directions. When you add these momentums together to find the total momentum of the two objects, you must consider the directions of those individual momentums. If the two momentums are exactly equal in magnitude but opposite in direction, they will cancel when you add them together and the total momentum will be exactly zero.

In a high bypass ratio turbofan engine, does the fan turn at the same RPM as the…

In a high bypass ratio turbofan engine, does the fan turn at the same RPM as the power turbine section — or is it geared down to run slower?

A turbofan engine uses a small turbojet engine to turn a giant fan and it is this fan that provides most of the engine’s propulsion. The question asks whether the fan is turned directly by the turbojet engine or whether gears are use to allow the larger fan to spin more slowly than the smaller turbojet. This is an interesting question, particularly since many of the parts inside a jet engine are spinning almost as fast as they can tolerate without ripping themselves apart.

A turbofan engine contains two separate rotating assemblies or “spools,” each of which is powered by hot exhaust gases flowing out of the combustion chamber through some turbine discs and each of which spins some compressor disc that push air toward the combustion chamber. The shorter of the two spools is hollow and the lower spool passes through its center.

The shorter spool, which spins at about 12,000 rpm, derives its power from high speed gas flowing through its turbine blades just after the combustion chamber and it powers a high pressure compressor just in front of the combustion chamber. The longer spool, which spins at about 4,000 rpm, derives its power from low-pressure gas flowing out of the high-pressure turbine and it powers both a low-pressure compressor in front of the high-pressure compressor and the actual turbofan blades. Overall, there is a rapidly turning hollow spool right around the combustion chamber and a more slowly spinning solid spool that extends both in front of and behind the high-speed spool. It’s the low speed spool that spins the turbofan itself.

If air in a turbofan engine bypasses the jet engine after going through the turb…

If air in a turbofan engine bypasses the jet engine after going through the turbofan, why does the jet engine even exist in the system?

The turbofan engine has a giant fan at its inlet, with a much smaller turbojet engine behind it. That turbojet engine is what provides the mechanical work needed to turn the giant fan. About 5 to 10% of the air passing through the fan then passes into and through the turbojet behind it. The turbojet uses this air for its operations: compressing it, burning fuel in it, and then extracting most of that hot air’s energy as rotational work. This rotational work is used to power the giant fan.

How does a gas turbine engine (i.e., an aircraft engine) work?

How does a gas turbine engine (i.e., an aircraft engine) work?

A gas turbine uses energy stored in pressurized or rapidly moving gas to do work on a rotating mechanism. This rotary work can then be used to propel a vehicle or to generate electricity. Whether the gas is pressurized or rapidly moving doesn’t really matter much. What is important is that the gas tends to flow from one region to another through a series of turbine blades. If the gas is pressurized, it is propelled through the blades by the unbalanced pressures (gases always accelerate toward lower pressure). If the gas is rapidly moving, it flows through the blades because of inertia.

As the gas flows through the turbine blades, it flows over and under each blade. The blades are shaped so that the gas goes faster over each blade than under each blade, and an imbalance of pressures results as a consequence of Bernoulli’s effect. Each turbine blade acts like the wing of an airplane and experiences a lift force. This lift force pushes on each blade and twists the turbine around and around. The turbine blades effectively fly through the flowing gas stream and extract energy from it. The blades and turbine gain energy while the gas stream loses energy. The gas leaves the turbine at a lower pressure and/or speed than it had when it arrived.

Please explain what “lift” is.

Please explain what “lift” is.

Suppose that a horizontal wind is approaching a smooth, stationary ball from the right. The ball will experience a drag force that pushes it toward the left. We call it a drag force because it acts to slow the ball’s motion through the air—in other words because it pushes the ball directly downwind. But if the ball isn’t uniform or if the ball is spinning, it may experience a force that isn’t directly downwind. If the ball experiences an aerodynamic force (a force due to the motion of the wind near its surface) that pushes it to the side, or that pushes it up or down, then it is experiencing a lift force. This lift force isn’t necessary up…it’s just to the side—at right angles to the downwind direction.

My big square truck creates a lot of turbulence when it moves. Does my roof rack…

My big square truck creates a lot of turbulence when it moves. Does my roof rack (a factory-installed one, close to the roof) actually improve aerodynamics, like fuzz on a tennis ball? (Also, what about the air dam at the back end?)

I’m sure that modern car designers consider aerodynamics when building a car or truck. They do structure the trailing edge of the car to minimize its turbulent wake. But I doubt that a roof rack helps much. It’s probably too tall for the boundary layer on the car and extends into the free flowing stream beyond. As a result, it probably experiences its own pressure drag. The “fuzz” that trips the boundary layer has to be no taller than the boundary layer itself, otherwise it causes turbulence in the main airstream rather than preventing it. The same goes for the air dam.