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DrGreg said:The clue is in the table headings.
It shouldn't be too difficult to work it out from that.
- "Thrust" is measured in Newtons.
- "Nozzle exit area" is measured in square metres.
- "Thrust density" is measured in Newtons per square metre.
Not really. It has units of force per unit area or, equivalently, of energy per unit volume. But unless you are also given something like the density (mass per unit volume) of the exhaust stream, it cannot tell you the exhaust velocity.AdrianHudson said:Ahh! So its the thrust produced per m2 of the nozzle area. Therefore that means that if you had nozzle "A" that has a surface area of 0.5m2 with a thrust of 10 Newtons and Nozzle "B" that has a surface area of 1m2 with a thrust of 10Newtons. Nozzle "A" is producing more thrust density?
Am I wrong in classifying thrust density as an efficiency of the given propulsion unit?
DrGreg said:
- "Thrust density" is measured in Newtons per square metre.
Thrust is a force that propels an object forward by pushing against a medium, such as air or water. It is typically measured in units of newtons (N). Thrust density is the amount of thrust per unit of area, typically measured in newtons per square meter (N/m²).
Thrust and thrust density are directly related, as thrust density is simply the thrust divided by the area over which it is applied. This means that as thrust increases, so does thrust density, and vice versa.
Thrust is commonly used in the field of aerospace to measure the force produced by jet engines or rockets. Thrust density, on the other hand, is more commonly used in fluid dynamics to analyze the flow of fluids and how they interact with surfaces.
No, thrust and thrust density cannot be used interchangeably as they measure different quantities. While thrust measures the overall force produced, thrust density takes into account the area over which the force is applied, providing a more specific measure of the force per unit area.
Changes in thrust and thrust density can greatly affect the performance of a system. An increase in thrust can result in a faster acceleration, while an increase in thrust density can result in a more efficient use of the available power. However, these changes must be balanced with other factors such as weight and drag to achieve optimal performance.