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Questions tagged [thrust]

Questions about the propulsive force of a powered aircraft.

5 votes
1 answer
701 views

How would an aircraft like the Tupolev Tu-154 “Careless”, the Boeing 727, or the Hawker-Siddeley Trident handle the loss of one of the rear mounted engines?
Drunk Hatsune Miku's user avatar
0 votes
1 answer
216 views

What would happen on a twin engine jet airliner like a Boeing 767-X00 series aircraft if one of the engines separated? In a normal one engine inoperative scenario the asymmetrical thrust and drag is ...
Drunk Hatsune Miku's user avatar
4 votes
3 answers
373 views

Here’s the rationale behind my question: The distance the CG is ahead of the NP determines longitudinal stability (technically it’s the derivative of pitching moments wrt AOA, but generally we end up ...
Cata's user avatar
  • 41
2 votes
1 answer
409 views

I have recently been sharpening up on my flying theory and have run into an issue with the power and thrust curves due to this question: Draw a graph showing the level flight power required and power ...
levi.r's user avatar
  • 23
3 votes
2 answers
855 views

Understanding that for a propeller driven aircraft, the airspeed for best endurance is the speed at which minimum power is required, and obviously the prop is more efficient at producing thrust at ...
Matt M's user avatar
  • 31
7 votes
7 answers
2k views

When a airliner takes off, it looks like after rotation and lift-off, the plane flies up in the air parallel to the length of its fuselage. Assuming lift from the wings is the major force in taking ...
slingeraap's user avatar
9 votes
1 answer
2k views

If you have two airplanes, one generating thrust directly with a jet engine, and the other generating thrust with a propeller (from any of its power sources i.e: ICE/piston, electric, etc), which one ...
gbe's user avatar
  • 8,571
1 vote
2 answers
229 views

I know for a fact that the extension of flaps shifts the thrust required/total drag curve higher. How do I prove mathematically that it also shifts to the left (LDmax with flaps extended occurs at a ...
Terry's user avatar
  • 669
0 votes
2 answers
394 views

I calculated the thrust and power of the helicopter to hover above the surface, but I'm not sure if I calculated correctly. I've already asked a similar question, but I've moved on, and there are more ...
Zippi's user avatar
  • 3
1 vote
2 answers
274 views

Curious of how many lbs/thrust can a single engine like the Socata TBM 900 (or a similar airplane) pull at sea level while parked at full thrust?
gbe's user avatar
  • 8,571
2 votes
1 answer
162 views

I have designed an aircraft and wanted to determine its performance charachteristics. the following parameters have been utilised: aircraft specifications: Mtow = 1.7kg wing_area = 0.411 m^2 Cl_max = ...
Curiousraptor's user avatar
2 votes
2 answers
557 views

I’m a high school physics student with an interest in aviation and would like to understand why commercial airplanes fly at high altitudes (e.g., 35,000 feet) to improve fuel efficiency. My ...
Sanjay Biswas's user avatar
0 votes
2 answers
218 views

Producing high thrust form jet engine is not one step. Actually, there are many factors that can significantly play rule here. Anyway, am focusing only on the nozzle side and its rule only in my ...
eeesa's user avatar
  • 171
1 vote
1 answer
278 views

In the PHAK, Chapter 5 Aerodynamics, the following statement is made regarding forces in a climb: The thrust required for a stabilized climb equals drag plus a percentage of weight dependent on the ...
Ryan BW's user avatar
  • 153
2 votes
1 answer
667 views

What are the tools, software or devices that jet engineers use to know if there is loss of pressure in the air? Are they using only calculations to know how much air in vs out? It's very interesting ...
eeesa's user avatar
  • 171

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