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why are jets faster then props? (Read 4697 times)
Feb 4
th
, 2003 at 11:02pm
ViNtAgE FlYa
Ex Member
why are jets faster then props? lol stupid question it may seem
but why??
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Reply #1 -
Feb 4
th
, 2003 at 11:24pm
Blade
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Ok, this is where it gets a tad bit complicated, so bear with me here. The propeller is spinning in the air right, thats ALOT of force on the blades, trying to pull them out, called centrifigal force. A propellor can only turn so fast. This is where the jet engine comes in. It has rows upon rows of blades, pushing the air back, so not as much strain on the blades compared to a prop. By doing this the jet blades can turn at much higher revs. Also accounting to the fact that you add fuel to the air and you ignite it, you get more added thrust by the heat. This is why a jet can go faster. But there are limits also, you can't go mach 6 with a jet engine, it reaches a limit also, so here comes the ram jet and scram jet. These two engines are similar but the scram jet has more power. Basically if you want to go really fast you use these. The ram jet is based on a deisel engine, there are no spark plugs. If you look straight through a ram jet engine, you dont see anything, it gets small in the middle, and then it gets bigger in the rear, there are no fan blades. What happens is that at high speed air is rammed, hence the name, down the intake, where it is compressed. As it is compressed, fuel is being added to the mixture as well. The intense amount of pressure causes the air to explode, and ignite the fuel, which propells the aircraft. If you remember the movie red october, with the catapiller drive, almost no moving parts, well this engine is the same thing but for the air, no moving parts. By using a ram jet, you can go infinite amounts of speed, BUT that all depends how long before the fuel runs out, or the plane rips apart around you. Below are some examples.
Jet Engines
http://inventors.about.com/library/inventors/bljetenginetypes.htm
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Feb 4
th
, 2003 at 11:33pm
Brett_Henderson
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Usually it's because, jet engines of the same weight as piston engines have more HP, thrust, wattage (or how ever else you measure power), but mainly it's because jet engines just keep applying accelleration until whatever load they're carrying reaches it's aerodynamic limit. Props (including turbo-probs) are like little wings trying to "climb" through the air, pulling the plane along. A prop can only cut through the air to a point, where a jet is constantly pushing, no matter how fast its moving.
Once you've eliminated the limits of the prop and have more airspeed to work with, you can get away with smaller wings, further increasing the aerodynamic efficiency of the plane, and you just keep getting faster
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Reply #3 -
Feb 5
th
, 2003 at 12:11am
Rifleman
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trying to overcome the drag induced by a propellor which has its root travelling sub-sonic and its tip travelling supersonic is the main limiting factor in why there is a limit to the airspeed obtainable for a propellor driven aircraft........drag is the biggest factor in Jet aircraft also.....drag climbs by a huge factor as airspeed increases......until we find a way to reduce this drag and raise the power level of our motive force, we will be still travelling around the same speeds as we do now in the air......in the vacuum of space, its a whole 'nother ball game !
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Reply #4 -
Feb 5
th
, 2003 at 9:18am
Brett_Henderson
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in the vacuum of space, its a whole 'nother ball game !
Yup, in a vacuum even the tiniest jet (rocket actually, as there is no air for the air/fuel mixture) could accelerate a 747 to incredible speeds. With no friction, the thrust vector (acceleration) just keeps accumulating in the form of velocity. However, you need to "turn around" when your 1/2 way to your destination and start "decelerating"
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Reply #5 -
Feb 5
th
, 2003 at 10:43am
Felix/FFDS
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Brett - you're wring, of course, haven't you seen the Star Wars movies? That's how its done...
Quote:
Yup, in a vacuum even the tiniest jet (rocket actually, as there is no air for the air/fuel mixture) could accelerate a 747 to incredible speeds. With no friction, the thrust vector (acceleration) just keeps accumulating in the form of velocity. However, you need to "turn around" when your 1/2 way to your destination and start "decelerating"
Felix/
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Reply #6 -
Feb 5
th
, 2003 at 2:52pm
Brett_Henderson
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Oh yeah, I forgot, how silly of me
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Reply #7 -
Feb 5
th
, 2003 at 7:37pm
Loafing Smurf
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Quote:
in the vacuum of space, its a whole 'nother ball game !
Yes, another ball game.
Airplane engines are called "breathing engines" because the fuel combust with the surrounding oxygen (in general fire needs oxygen) In space, chemical rockets need an oxidizer to complete the combustion with fuel.
Let me take you through a general process of the rocket engine.
*ranger sings in the tune of that bone song. (you know, "the hip bone is connected to the.....')*
The fuel and oxidizer is pumped into the injectors, the injectors causes vaporization. Then the vaporization causes mix-ing. The mixing is ignited by the igniters. The igniters causes combustion. The combustion produces hot ga-ses. The hot gases go trough the nozzle. And then hotthrustprducinggasses comes out.
*note* Igniters and nozzle are not in the diagram.
Thats just a liquid fueled rocket in the chemical category.
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Reply #8 -
Feb 5
th
, 2003 at 8:39pm
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trying to overcome the drag induced by a propellor which has its root travelling sub-sonic and its tip travelling supersonic is the main limiting factor in why there is a limit to the airspeed obtainable for a propellor driven aircraft........drag is the biggest factor in Jet aircraft also.....drag climbs by a huge factor as airspeed increases......until we find a way to reduce this drag and raise the power level of our motive force, we will be still travelling around the same speeds as we do now in the air......in the vacuum of space, its a whole 'nother ball game !
I want to add on to this. Another thing is the vacuum trail. When a propeller spins, it creates forward thrust. When the fan spins in a jet engine, it creates foreward thrust. What it also does, is at the exhaust, it creates a whilrpool effect. When it hits the tail, has less friction with the air molecules, thus, less drag.
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Reply #9 -
Feb 5
th
, 2003 at 9:35pm
katana_1000
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Yup, in a vacuum even the tiniest jet (rocket actually, as there is no air for the air/fuel mixture) could accelerate a 747 to incredible speeds. With no friction, the thrust vector (acceleration) just keeps accumulating in the form of velocity. However, you need to "turn around" when your 1/2 way to your destination and start "decelerating"
and exactly how do you decelerate in an enviorment with no air if u have one little rocket engine pushing the plane forward?(first person to explain this gets a shiny new quater and a shiny new learjet;)
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Reply #10 -
Feb 5
th
, 2003 at 9:53pm
Loafing Smurf
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and exactly how do you decelerate in an enviorment with no air if u have one little rocket engine pushing the plane forward?(first person to explain this gets a shiny new quater and a shiny new learjet;)
If a thruster applies force directly opposite of the direction it is moving, it should slow down. Objects with more momentum would require more force to slow down an object in space.
That lear jet sounds mighty tempting, but I'll take the quarter. LOL...I just wanted to say that, even if the anwser is wrong.
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Reply #11 -
Feb 5
th
, 2003 at 10:05pm
Deputy
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I cant think much of a better analogy right now, because of my son. . .
Think of a skateboard. Push it on a flat level surface. Its moving, so how is it going to stop? Either it will hit something, or a constant opposite reaction (gravity) will slow it down. In space, a small can of oxygen could easily stop the shuttle in space. It has a constant equal and opposite reaction.
Newton's Law applies here - For every action, there is an equal and opposite reaction.
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Reply #12 -
Feb 5
th
, 2003 at 11:41pm
Rifleman
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" Full size A/C are just
overgrown models ! "
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Quote:
Yes, another ball game.
Airplane engines are called "breathing engines" because the fuel combust with the surrounding oxygen (in general fire needs oxygen) In space, chemical rockets need an oxidizer to complete the combustion with fuel.
Let me take you through a general process of the rocket engine.
*ranger sings in the tune of that bone song. (you know, "the hip bone is connected to the.....')*
The fuel and oxidizer is pumped into the injectors, the injectors causes vaporization. Then the vaporization causes mix-ing. The mixing is ignited by the igniters. The igniters causes combustion. The combustion produces hot ga-ses. The hot gases go trough the nozzle. And then hotthrustprducinggasses comes out.
*note* Igniters and nozzle are not in the diagram.
[img]
Thats just a liquid fueled rocket in the chemical category.
One upgrade to the whole idea you present here....in the event of the little boy crouchng under the nozzle trying to strike his match to light the fuel and oxidizer, and winding up finding the sulphur all paste from moisture, they now use a foolproof method of ignition,....the fuel and oxidizer are " hypergolics ".....materials which ingite on contact with each other........been using these types since leaving the moon became a requirement to a successful mission.
oh yeh, one more thing..... airplane engines are called "
air
breathing engines"
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Reply #13 -
Feb 6
th
, 2003 at 12:17am
Brett_Henderson
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and exactly how do you decelerate in an enviorment with no air if u have one little rocket engine pushing the plane forward?(first person to explain this gets a shiny new quater and a shiny new learjet;)
I said, "Turn around" , or turn the engine around (thrust pointing in opposite direction),,geez
Can I have the quarter ?
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Reply #14 -
Feb 6
th
, 2003 at 2:45am
Cloud Maker
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Interesting replies here. I'm surprised that nobody mentioned
stall speed
. Jet engines, having more blades per row and more rows are more efficient at moving air than propellers. About the best a prop can do is use a countr-rotating system. Because props are so inefficient they have a tendency to stall around mach1 due to compression of the air in front of the blades. Jet engines stall too, but it takes a more severe event, such as introducing hot gas to them. Hot air being more sparse will play hell with a fast spinning turbine blade, causing a compressor stall. If your lucky, the engine will re-ignite. If not, well...................
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Reply #15 -
Feb 6
th
, 2003 at 8:04am
Brett_Henderson
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Interesting replies here. I'm surprised that nobody mentioned stall speed . Jet engines, having more blades per row and more rows are more efficient at moving air than propellers
Hmmm, thought I "kinda" said that :
Quote:
Props (including turbo-probs) are like little wings trying to "climb" through the air, pulling the plane along. A prop can only cut through the air to a point
I still want my quarter.
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Reply #16 -
Feb 6
th
, 2003 at 9:41am
Felix/FFDS
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To add what Brett said -
assume you have a rocketship at rest in space...
If you accelerate from a full rest at a constant 1.0g for 24hrs ... shut the engine off ... coast (at the final speed reached ... you will need to turn the rocketship 180degrees so that the thrust will point in the exact direction of the line of travel and turn it on again for 24hrs at a 1.0g acceleration to come to a complete stop.
It's a matter of vector math - x force at y angle applied can be stopped by x force at -y angle... or forces b at angle -u, c at angle -v as long as their vector sum equal force x at angle -y ...
Quote:
and exactly how do you decelerate in an enviorment with no air if u have one little rocket engine pushing the plane forward?(first person to explain this gets a shiny new quater and a shiny new learjet;)
Felix/
FFDS
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Reply #17 -
Feb 6
th
, 2003 at 10:25am
Brett_Henderson
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Anyone in my age bracket (40+) surely played Asteriods in the arcades.
That game was a perfect example of how vector math applies to a rocket. Remember when you would run from the little saucer as fast as the ship would fly ? And then when it was safe, you'd have to turn the ship around and apply the thrust just to slow down and gain control.
And that was only on 2 dimensions, imagine trying it in a "3-D" environment
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Reply #18 -
Feb 6
th
, 2003 at 11:04am
Rifleman
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this stall you are talking about in front of a propellor is what I was referring to when I addressed the difference in the tip and root speeds of a prop....tips hit Mach 1 faster than root, .....thats the noise we here from a high speed Heli.....as for the cpmpressor stalls, from high density air being forced down the throat of modern jets, thats the reason the variable intake was brought into play....remember the performance of the B-1 ? before the variable intakes and exhausts were removed on this bird to reduce costs, and produce the B-1B
, the B-1A was a much higher performance aircraft.....much faster !............backin ya up 100% on this one
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Reply #19 -
Feb 6
th
, 2003 at 3:24pm
katana_1000
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Hmmm, thought I "kinda" said that :
I still want my quarter.
ok,ok*gives brett his damn quater*
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Reply #20 -
Feb 6
th
, 2003 at 3:54pm
ViNtAgE FlYa
Ex Member
wow, i never expected to get this much of a responce....
i've lernt more then i do in school in 2 weeks!!! well maybe i should be paying more attention in school...
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Reply #21 -
Feb 7
th
, 2003 at 6:09am
Professor Brensec
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I said, "Turn around" , or turn the engine around (thrust pointing in opposite direction),,geez
Can I have the quarter ?
Any of the brighter designers would have "retro" (meaning reverse or backwards) rockets or engines already facing the other way!!
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Reply #22 -
Feb 7
th
, 2003 at 8:50am
Brett_Henderson
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I love how these threads take on a life of their own
Quote:
Any of the brighter designers would have "retro" (meaning reverse or backwards) rockets or engines already facing the other way!!
I dunno,, since we've jumped over from "prop vs. jet" to "space-travel", let's ponder it.
A retro-rocket capable of counter-acting the velocity built up by another rocket, would have to be at least as big, powerful and heavy. That would make it "dead weight" for 1/2 the flight.
Small maneuvering rockets (to turn around) or a mechanical sytem to reverse the main rocket (or it's thrust) is more the way to go.
Can't wait to see where this thread goes next ???
PS. "dead weight" should read, "dead mass", as there is no weight without gravity
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Reply #23 -
Feb 7
th
, 2003 at 9:08am
Felix/FFDS
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Yes, it's more efficient to use smaller maneouvering thrusters than another "equal and opposite" rocket.
As to mechanical means - an internal "flywheel" type arrangement could be considered, using the torque of a spinning mass to rotate the overall ship. I think, however, that given the masses involved, thrusters are more efficient.
(Where Andy Libby when we need him?)
Quote:
I love how these threads take on a life of their own
I dunno,, since we've jumped over from "prop vs. jet" to "space-travel", let's ponder it.
A retro-rocket capable of counter-acting the velocity built up by another rocket, would have to be at least as big, powerful and heavy. That would make it "dead weight" for 1/2 the flight.
Small maneuvering rockets (to turn around) or a mechanical sytem to reverse the main rocket (or it's thrust) is more the way to go.
Can't wait to see where this thread goes next ???
PS. "dead weight" should read, "dead mass", as there is no weight without gravity
Felix/
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Feb 7
th
, 2003 at 10:49am
Rifleman
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" Full size A/C are just
overgrown models ! "
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Quote:
let's ponder this......
A retro-rocket capable of counter-acting the velocity built up by another rocket, would have to be at least as big, powerful and heavy. That would make it "dead weight" for 1/2 the flight.
PS. "dead weight" should read, "dead mass", as there is no weight without gravity
Brett, first thing to ponder...why would it be necessary to carry a slower-downer the same size as the giddy-upper.......if its half the size, then you just run it twice as long ?
so you take twice as long to slow down....... one third of the trip accelerating and two thirds in the de-celerate mode !
As for "Dead Weight" being changed to read "Dead Mass" ?...whats the difference ?....Mass is defined as the "unit of weight per unit of volume "......gee theres that weight thing again.....I think it(using the term weight) has something to do with the amount of potential energy and kinetic energy and the managment of both........its just that we express the requirements of both, the amount of force to move a body or to resist the bodys motion, in a common way......1 lb of thrust can accelerate a 1 lb body at a given rate, and, if aimed in the direct opposite direction of travel, will de-celerate it at the same rate......in a vacuum, of course .
Am I confused yet ?
ps: and to keep on topic, this motive force can be generated in air too by a propellor 8)
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Reply #25 -
Feb 7
th
, 2003 at 2:42pm
Brett_Henderson
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Brett, first thing to ponder...why would it be necessary to carry a slower-downer the same size as the giddy-upper.......if its half the size, then you just run it twice as long ? so you take twice as long to slow down....... one third of the trip accelerating and two thirds in the de-celerate mode !
That's the point,, you don't want 2 at all. You want to use 100% of your engine mass accelerating/decelerating,, any deviation from that adds time to the trip (geometrically I might add).. the shortest possible trip would be accelerating full speed to the 1/2 way point, and then decelerating to a stop.
Quote:
As for "Dead Weight" being changed to read "Dead Mass" ?...whats the difference ?....Mass is defined as the "unit of weight per unit of volume
I believe you're confusing "mass" with "density"...
Weight is a function of Mass X Gravity .. on Earth that gravity equals (32'/sec^2)
Kilograms and Pounds can only be linearally converted on Earth..
'Kilograms' are units of Mass,, the English-system equivelant is the 'Slug'...
Pounds are units of force (Mass X Gravity),, the Metric-system equivelant is the 'Newton'...
Ever notice that rocket thrust is always given in either 'pounds' or 'newtons', never 'kilograms' ?
I believe the moon's gravity is 1/6 that of Earth, so here goes the comparison:
An object weighing 6 pounds on Earth weighs 1 pound on the moon.... An object with 6 kilograms of mass on Earth STILL has 6 kilograms of mass on the moon .
Or,, carried to the extreme.. in zero gravity nothing "weighs" anything,, everything still hass "mass"
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Reply #26 -
Feb 7
th
, 2003 at 7:55pm
Loafing Smurf
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Quote:
One upgrade to the whole idea you present here....in the event of the little boy crouchng under the nozzle trying to strike his match to light the fuel and oxidizer, and winding up finding the sulphur all paste from moisture, they now use a foolproof method of ignition,....the fuel and oxidizer are " hypergolics ".....materials which ingite on contact with each other........been using these types since leaving the moon became a requirement to a successful mission.
oh yeh, one more thing..... airplane engines are called "
air
breathing engines"
I stand corrected.
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Reply #27 -
Feb 7
th
, 2003 at 8:32pm
Rifleman
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" Full size A/C are just
overgrown models ! "
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I did say that I could be confused !.....it does explain one thing, though.....it takes less time to get home from the moon than it does to go there......its all downhill(relatively speaking), with only one sixth of the escape velocity required to break free of the moons influence and allow the earths to take over.....5/6ths of the trip back is accelerating.....without further motive force being applied internally at the vehicle........I guess thats why long distance space travel so far, has made use of other celestial bodies and their imparted gravitational influence to the traveller............Americans call it the singshot effect.....in England a slingshot is a catapult .
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Reply #28 -
Feb 7
th
, 2003 at 8:36pm
Deputy
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Quote:
Yes, it's more efficient to use smaller maneouvering thrusters than another
"equal and opposite"
rocket.
As to mechanical means - an internal "flywheel" type arrangement could be considered, using the torque of a spinning mass to rotate the overall ship. I think, however, that given the masses involved, thrusters are more efficient.
(Where Andy Libby when we need him?)
I assumed we were talking about inside the atmosphere. . .
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Reply #29 -
Feb 8
th
, 2003 at 5:53am
Professor Brensec
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Can't you give me a couple
more inches, Adam?
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Quote:
A retro-rocket capable of counter-acting the velocity built up by another rocket, would have to be at least as big, powerful and heavy. That would make it "dead weight" for 1/2 the flight.
We were talking about a Jumbo being moved through space by "the tiniest rocket". This is what I based my comment on. Another "tiny one" would not make that much difference. In fact, depending on the definition of "tiny", it may even have less mass than the thrusters you speak of.
As once a rocket propelled object reaches it's required velocity and remains at that velocity until acted upon by some opposite force (inertia), the extra weight (little as it is) I don't feel would make a difference in this particular scenario.
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Reply #30 -
Feb 9
th
, 2003 at 11:39pm
SilverFox441
Ex Member
Jet engine turbines don't stall because of the configuration of the intakes. The intake is designed to slow the incoming airstream and increase it's pressure.
Some aircraft (like the SR-71) have variable geometry intakes that allow this effect to be maintained over a wider speed range. You should note that the SR-71 and the F-104 (which had a similar intake style) both suffered from "unstarts" which is basically a compressor stall caused by allowing supersonic airflow into the engine.
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Reply #31 -
Feb 10
th
, 2003 at 12:44am
Deputy
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Which would cool the air enough that it couldnt cause thrust right? I should know this, but I don't.
-Brad
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Reply #32 -
Feb 10
th
, 2003 at 10:02am
Felix/FFDS
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Without going into details, combustion turbines (i.e., gas turbines, but considering they can operated on fuel oil, propane, natural gas, ....) are designed to operate at a certain range of inlet air mass/pressure - too much or too little air flow and your turbine won't turn over...
(analogy -stand in the airflow of a table fan - if it's turning fast enough, you won't be able to breathe properly... too much air for you to handle, so you have to take it in "gulps; get on a high mountain, where there's lower air pressure ("thin air") and you can't breathe either - you'll welcome that table fan!)
This is one of the reasons you have variable inlets - to control the airflow into your turbine
The air temperature is important - the compressor takes in the inlet air, increases the pressure and by pressurizing it, increases the temperature so that when it goes into the combustion chambers, and fuel is injected and ignited, a more efficient combustion takes place...more *work* is generated to turn the turbine blades which turn the compressor.....
In a pure tubojet engine, the thrust provided by the exhausted gases (the jets) provides all the force.
In high bypass engines, the "fans" up front provide most of the "thrust"
You can generalize up to a certain point - all combustion turbines "suck, squeeze, bang, and blow" - its the how they do it that drives engineers nuts...(who have to start with)
Quote:
Which would cool the air enough that it couldnt cause thrust right? I should know this, but I don't.
-Brad
Felix/
FFDS
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Reply #33 -
Feb 15
th
, 2003 at 10:24am
Fly2e
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Global Moderator
It's 5 O'clock Somewhere!
KFRG
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Yeah, I agree with
and
and
and
! Thanks for info. I am going back to the garage and make a few adjustments to the jet engine I am building! Now, if only I could find where I put those directions! LOL
Intel Core i7 Extreme Processor 965, 4.2GHz/8MB L3 Cache, Asus P6T Deluxe V2 Intel X58 Chipset Cross
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Reply #34 -
Feb 15
th
, 2003 at 2:36pm
Deputy
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Hillsboro, Oregon
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Quote:
Without going into details, combustion turbines (i.e., gas turbines, but considering they can operated on fuel oil, propane, natural gas, ....) are designed to operate at a certain range of inlet air mass/pressure - too much or too little air flow and your turbine won't turn over...
(analogy -stand in the airflow of a table fan - if it's turning fast enough, you won't be able to breathe properly... too much air for you to handle, so you have to take it in "gulps; get on a high mountain, where there's lower air pressure ("thin air") and you can't breathe either - you'll welcome that table fan!)
This is one of the reasons you have variable inlets - to control the airflow into your turbine
The air temperature is important - the compressor takes in the inlet air, increases the pressure and by pressurizing it, increases the temperature so that when it goes into the combustion chambers, and fuel is injected and ignited, a more efficient combustion takes place...more *work* is generated to turn the turbine blades which turn the compressor.....
In a pure tubojet engine, the thrust provided by the exhausted gases (the jets) provides all the force.
In high bypass engines, the "fans" up front provide most of the "thrust"
You can generalize up to a certain point - all combustion turbines "suck, squeeze, bang, and blow" - its the how they do it that drives engineers nuts...(who have to start with)
Oh thanks, that makes me feel smart. . .
-Brad
Bad boys, bad boys, whatcha gonna do? Whatcha gonna do when I come for you?&&&&
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Reply #35 -
Feb 19
th
, 2003 at 5:39pm
torquestripe
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Need to Know Basis
Posts: 133
Because the air speed indicator says so!!! Jeez Loweez.
Save your brain cells for the HARD questions like why is the grass green or why is the sky blue.
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Reply #36 -
Feb 19
th
, 2003 at 11:04pm
Professor Brensec
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Can't you give me a couple
more inches, Adam?
SYDNEY - AUSTRALIA
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As you see, the comment has been completely removed.
Thanks, no harm.
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Reply #37 -
Feb 19
th
, 2003 at 11:05pm
torquestripe
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Need to Know Basis
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Reply #38 -
Feb 19
th
, 2003 at 11:12pm
Professor Brensec
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Colonel
Can't you give me a couple
more inches, Adam?
SYDNEY - AUSTRALIA
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Posts: 2955
Quote:
OH gosh almost forgot, could you please direct me to one of the more enlightened forums.
Pretty much any of the others. This one is unique, in that it's populated almost exclusively by people with IQ's Higher than "cretin"
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cried because I had no shoes - until I saw a man who had no feet.&&&&Dell Dimension 8100 - Intel P4 1.7 Gb - 512 RD Ram - nVidia GeForce 128 mb FX5200.
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Reply #39 -
Feb 26
th
, 2003 at 3:46am
Redsunfox
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" American Airlines may
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North Dallas, Texas
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Hi All,
The only stupid question, is the question you don't ask.
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