Questions tagged [turbojet]
A type of jet engine where all the air passing through the engine is used to burn fuel and drive a turbine as well as generating thrust.
58
questions
1
vote
2
answers
81
views
Why are inlet and outlet (exhaust) pressure considered to be the same in a turbojet engine?
Why do we take outlet/exhaust pressure (station 6) as the same as in inlet (station 1) ?
In T-S diagram, we see that outlet temperature is much higher than inlet temperature since flow in outlet has ...
- 161
1
vote
1
answer
68
views
Where is the thrust of a turbojet felt? [duplicate]
At a high level, this is simple. Hot gas goes out the back, and Newton's third law says the engine is pushed forwards. But when you look inside the engine, it's less clear which part experiences the ...
- 522
7
votes
5
answers
2k
views
How do gas turbine engines and turbofan engines keep constant compressor side rpm?
How do the RPMs stay constant in a gas turbine engine? For example in car with piston engine, when you keep pressing the accelerator the rpms keep picking up, to keep the rpms constant you must let ...
- 263
4
votes
1
answer
194
views
Why the green inside newer turbofan engine nacelles?
What is the purpose of the recent phenomenon of green being seen inside newer turbofan engine nacelles, just to the front of the fan blades?
- 61
2
votes
1
answer
191
views
MIG 29 Engine - how to interpret these values?
I was wondering how powerful the engines of the MIG 29 are. On Wikipedia I found some specifications for it.
How is the mass flow rate calculated? I know mass flow rate = density * area * velocity.
...
- 29
1
vote
1
answer
374
views
Logging Dual Received in a Single-Pilot Turbojet, FAA
Can you log dual received in a single-pilot turbojet on Part 91 flights if the PIC is type-rated, holds a valid MEI and instruction is being given?
Can the AMEL-rated student log AMEL category and ...
5
votes
3
answers
3k
views
How come a turboprop can't reach speeds as high as a turbofan?
I understand that turbofan powered aircraft can reach much faster speeds than turboprops like the C130 Hercules, and I can't imagine a turbofan turboprop powered 737 would be of any use really, but as ...
- 51
4
votes
1
answer
489
views
Early turbojet RPM and thrust indicator
The flight operations handbook for the Douglas X-3 Stiletto (an experimental aircraft from the early 1950s) says that the instrument panel has instruments that indicate the thrust of the two ...
- 716
2
votes
2
answers
205
views
How does a turbojet engine's performance change as the load on it varies? [closed]
What happens when the load increases on the turbojet engine? What senses the speed change in jet engines and how speed correction takes place?
- 21
4
votes
2
answers
209
views
What does "military band" mean in this chart?
I'm reading the manual of J79 engine, and I just saw this chart:
Does anybody know what "military band" means?
- 3,237
0
votes
1
answer
198
views
Why does J79 have speed more than 100%? [duplicate]
In the maintenence manual of J79 saw this table:
As you can see, there is speed more than 100% and it looks that the engine can handle it. Can't it?
One more thing, days ago, watched this movie: ...
- 3,237
4
votes
2
answers
1k
views
What does "time at temperature" mean in the maintenance manual of the J79 engine?
I was reading the maintenance manual of the General Electric J79 and saw these two charts:
and
What does "time at temperature" mean?
- 3,237
1
vote
1
answer
111
views
Is axial bearing in turbo fan,turbo jet engines neutraly loaded?
Is axial bearing in turbo fan,turbo jet engines neutraly loaded,if yes then turbine/fan and compresor produce eqaul and opposite force?
If yes ,where then thrust come from,at internal walls,must be ...
- 1,563
2
votes
1
answer
212
views
Do aircraft engines come with electric generators?
For turbojet/fan/prop engines, do they come with an electric generator when delivered to aircraft manufacturers, or it is something that the aircraft manufacturer has to find or make themselves?
I am ...
- 583
6
votes
2
answers
298
views
Do turbine engines contain engine oil and fire-extinguishing fluid?
When aircraft turbine engine companies sell their engines to aircraft manufacturers, does the product contain the tank and pipe for engine oil and fire extinguishing fluid in the same package? Or is ...
- 583
2
votes
2
answers
2k
views
Do jet fighters use Turbojet engines, and do cargo/passenger aircraft use Turbofan engines? [duplicate]
I have a feeling that Turbofan engines are used in jet fighters and Turbojet engines are used in cargo or passenger aircraft.
Is my perception correct?
Do jet fighters use Turbojet engines?
Do cargo/...
- 834
2
votes
0
answers
147
views
Overheating (fire thrown out of the nozzle) [closed]
At first I copied https://www.jetcat.de/en/productdetails/produkte/jetcat/produkte/hobby/Engines/P160_rxi_b
Where I manufactured and installed all the parts and they are very similar to the original ...
- 29
4
votes
3
answers
1k
views
How are compressor disks connected to the shaft?
I am trying to learn how compressor disks and shaft are connected each other. I don't have any idea about the terminology so I couldn't find anything useful.
Here is a section view of a sample and I ...
- 101
1
vote
3
answers
218
views
Are there aircraft with multiple inlets for a turbojet engine?
Are there aerial vehicles which have multiple inlets with air ducts (shaped in S-forn) , which all lead the air to one single turbojet engine?
I have not enough space to put just one inlet area on my ...
- 61
1
vote
2
answers
2k
views
Why is the fuel:air ratio of a turbojet engine not around ~1:15 (the stoichiometric ratio)? [closed]
Also, what is the maximum fuel:air ratio possible in a combustion chamber of a jet engine?
- 23
1
vote
2
answers
326
views
Does airspeed impact fuel flow?
Let's say an F-104 Starfighter is flying at sea level at 600 KIAS with throttle at 100% RPM.
Then, let's say the F-104 is still flying at sea level, but the pilot reduces throttle and airspeed falls ...
- 101
7
votes
1
answer
1k
views
What causes the horn-like noise during the start-up of some jet engines?
Here's the specific sound I'm talking about (it starts specifically 56 seconds into the video, as well as at 2:02 for the second engine):
I've only really heard that ...
- 73
3
votes
2
answers
217
views
Is the well known textbook-formula for net-thrust oversimplified or do I have a misinterpretation?
In order to understand how Jet-Engines works I came across the "famous" formula for net-thrust:
https://en.wikipedia.org/wiki/Turbojet#Net_thrust
$F_{thrust} = Q_{out} \cdot v_{out} - Q_{in}\...
- 241
9
votes
5
answers
4k
views
Do jet aircraft have a better glide ratio than propeller aircraft in general? If so, why?
Being fond of aviation, I play with software simulators a lot.
I have noticed that while jets seem to be able to glide for a long distance even at zero throttle, propeller aircraft need to be ...
- 467
6
votes
1
answer
3k
views
Can you identify this engine?
I am studying Aircraft mechanics currently, and in our academy we have some aircraft engines and different types of them, and I need please your help to know the reference of one of them, and if it is ...
- 79
2
votes
1
answer
464
views
KSEE LOC-D conundrum
Consider the LOC-D at KSEE and note the Alternate Minimums criteria.
99.9% of the time, the winds strongly favor 27R;
The tower closes at 1900 PT currently (usually at 2100 PT non COVID times);
LOC-D ...
- 927
0
votes
1
answer
2k
views
How do I find out the fuel consumption of the PT6A for a lightly loaded aircraft?
The Fuel consumption of PT6 engines provided by manufacturers are as follows.
Cessna Caravan - Consumption ~47? GPH. At full load at ~160? Kn.
Quest Kodiak - Around 49 GPH at full load at ~170 Kn
...
user46196
2
votes
2
answers
675
views
Is it true that high-bypass engines are inherently inefficient at higher speeds?
Power consumption=Kinetic energy=$1/2mv^2$.
Thrust=momentum change=$mv$.
I keep being told that aircraft engines are most efficient when their exhaust velocity closely matches the freestream.
The ...
- 3,400
2
votes
1
answer
1k
views
Does jet engine exhaust velocity relative to itself remain constant despite speed changes?
Maybe this is a stupid question.
I seem to have been told, the velocity of the exhaust leaving an airbreathing jet engine relative to the engine, is constant despite changes in airspeed. However, to ...
- 3,400
-2
votes
1
answer
310
views
Rocket Thrust vs Air breathing jet engine why is a rocket better [duplicate]
What are design dynamics that give the rocket engine higher thrust than an air breathing jet engine of similar size in comparison to a turbo jet engine, turbo fan engine, high by pass turbo fan engine,...
- 8,469
1
vote
0
answers
160
views
How do the contrarotating turbines work in the F-119-PW-100?
I was reading about the F22 Raptor and found out that its powerplants use contrarotating turbines. How does this work
Also, if the spools and their connected compressors are rotating in opposite ...
- 11
4
votes
1
answer
475
views
Why did the B-52 never have a JT4A-powered version?
All versions of the B-52 use the Pratt & Whitney JT3C turbojet (except for the last version, the B-52H, which uses the JT3D low-bypass turbofan instead).
Problem: the JT3C is a horribly anemic ...
- 27.5k
25
votes
8
answers
50k
views
What is the difference between turbojet and turbofan engines?
What is the difference between a turbojet engine and a turbofan engine?
I know that both of them have a fan and have turbines but how to distinguish them?
9
votes
3
answers
4k
views
Why is thrust available constant with speed for turbojet engines, when it varies with speed for turboprop engines?
Similarly, why is power available (nearly) constant with speed for a propeller engine, while it varies for a jet engine?
- 309
1
vote
1
answer
1k
views
What is the air/fuel mixture ratio in a turbojet engine?
How does it relates to stoichiometry ? What are the possible extinction accidents related to air/fuel mixture ratio ?
- 275
1
vote
2
answers
437
views
How does an engine work when an airplane has $v=0$ on the ground?
I mean, for a turbofan:
$$ T= \dot m_{air,h} (1+f) v_{e,h}+ \dot m_{air,c} v_{e,c}- (\dot m_{air,h}+ \dot m_{air,c} ) v_0+ (P_{e,h}-P_{amb} ) A_{e,h}+ (P_{e,c}-P_{amb} ) A_{e,c} $$
but
$$ \dot m_{air}...
- 53
1
vote
3
answers
508
views
Can a gas turbine be able to switch from torque to thrust?
Can a turbine engine be switched from providing torque (like a helicopter) to the rotor to transfer power to provide exhaust thrust (like a jet plane)?
Related: BV-347 upgrade this way?
- 1
0
votes
1
answer
150
views
Why can't turbojets or turbofans be overtemped or overtorqued the way turboprops can?
Turboprops that aren't FADEC controlled can be overtorqued or overtemped if the power lever is moved too far forward yet I have never heard of a jet that can't be "firewalled", FADEC or not. Why is ...
- 11
13
votes
2
answers
2k
views
Are centrifugal turbojets easier to make than axial ones?
Looking at the history of jet engines, I noticed that the British first made centrifugal-types, but the Germans went straight into axial-types.
Which type is easier, if any? By that I mean, which ...
- 17.4k
0
votes
1
answer
6k
views
What is significance of N1 and N2 in Jet engine? [duplicate]
Why N1 Low pressure compressor RPM and N2 High Pressure compressor RPM are monitored in jet engines ?
Why specifically compressor RPM rather than turbine RPM ?
What do N1 and N2 signify in terms of ...
- 514
28
votes
8
answers
7k
views
Why do we refer to "power" for turboprop engines and "thrust" for turbojet/fan engines?
In jet engines, I read that thrust is related to the fuel flow rate, whereas in turboprop engines power produced is related to the fuel flow rate. What is the reason and brief math behind this?
- 514
10
votes
2
answers
2k
views
When were the last subsonic turbojet-powered airliners retired from commercial passenger service?
The very first jetliners (Comet, Tu-104, Caravelle I-VI, 707-120/-220/-320, DC-8 series 10-30, original 720, CV-880) all used turbojet engines, turbofans not being available until later; when ...
- 27.5k
3
votes
1
answer
728
views
What is the difference between active tip clearance control system and passive tip clearance control system in turbine?
What are the main differences between turbine active tip clearance control system and passive tip clearance control system?
- 33
0
votes
3
answers
2k
views
Why does a turbine engine compressor ratio affect stagnation pressure?
This might just be a misunderstanding on my part, but in an ideal Brayton cycle, the flow through the compressor and turbine is isentropic, meaning $\Delta s = 0$. However, usually you are given the ...
- 175
2
votes
4
answers
1k
views
How can I determine specific heats of gases for turbojet engine calculations?
I'm in a combustion lab and we are performing experiments on a turbojet engine. However, I am having some trouble calculating the exit velocity and compressor/turbine powers of the engine.
Consider ...
- 175
2
votes
2
answers
645
views
Can a turbojet jet or turbofan powered aircraft land and take off from water?
Can a turbojet jet or turbofan powered aircraft land and take off from water? How much clearence from the water surface would it need for its engines so that it does not suck up water?
- 8,469
7
votes
2
answers
604
views
What exactly does the MB-326's 'relight' button do?
The following picture shows the engine throttle of an Aermacchi MB-326, which is powered by the Rolls-Royce Viper turbojet:
(source - all photos © Drive&Fly Model Club)
I wonder what exactly the ...
- 579
1
vote
2
answers
135
views
Fans of tubofan jet engines
Does the thrust of the fan in a turbofan jet engine decrease proportionally with decrease in the diameter of the fan?
As the fan in a jet engine is responsible for over 70% of the total thrust can a ...
- 19
18
votes
1
answer
18k
views
Which jet engines have the highest thermal efficiency?
Some automakers (Mercedes-Benz, Toyota) have recently been making news about the improved thermal efficiency of their engines, stating that they reached the 50% mark. I was wondering if it was the ...
- 912
2
votes
1
answer
1k
views
Are there any differences between turbofan and turbojet engines besides bypass air? [duplicate]
I think I understand both engine types, but I am just wondering am I right in saying that the only difference between the two types of engines is the bypass air (i.e. a turbofan is just a turbojet ...
- 165