Divergent Nozzle Homework: Integrating to Get 5

In summary, there may be a discrepancy in the equation due to a missing 0.5, but further research is needed for clarification.
  • #1
TimeRip496
254
5

Homework Statement


upload_2017-12-12_0-14-50.png
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where the boldface type denotes a vector quantity. In general, the incremental surface dS may be expressed as r dψ R d∅. Examining Figure 1, we see that dS = R2 sin∅ dψ d∅ for this particular nozzle. Substituting Equations 3 and 4 in Equation 2 and integrating ∅ from zero to θ and ψ circumferentially from zero to π, we arrive at the result
upload_2017-12-12_0-14-29.png


Homework Equations

The Attempt at a Solution


When I integrate to get 5, I get 0.5ρve2R2sin2θ instead. Shouldn't there be a 0.5 when you integrate sinθcosθ or did the paper miss out on something?

Source: https://mdao.grc.nasa.gov/publications/NASA-TM-105176-Diverge.pdf
 

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  • #2
It is possible that there is a typo in the paper and the 0.5 is missing. However, it is also possible that the 0.5 was intentionally left out because it cancels out when the equation is simplified. Without more context or information, it is difficult to determine the reason for the discrepancy. It may be helpful to double check your integration and also consult other sources for the correct equation.
 

1. What is a divergent nozzle?

A divergent nozzle is a type of nozzle that widens towards the exit. It is used in fluid dynamics to accelerate the flow of a fluid, such as air or water, by converting the pressure energy into kinetic energy.

2. How does a divergent nozzle work?

A divergent nozzle works by increasing the cross-sectional area of the flow, which decreases the pressure and increases the velocity of the fluid. This is based on the principle of conservation of energy, where the decrease in pressure is offset by an increase in kinetic energy.

3. What is the purpose of integrating to get 5 in "Divergent Nozzle Homework"?

The purpose of integrating to get 5 in "Divergent Nozzle Homework" is to calculate the total pressure ratio across the divergent nozzle, which is equal to 5. This is an important parameter in fluid dynamics and is used to determine the performance of the nozzle.

4. What are the steps involved in integrating to get 5 in "Divergent Nozzle Homework"?

The steps involved in integrating to get 5 in "Divergent Nozzle Homework" include:
1. Expressing the pressure and velocity equations in terms of the Mach number
2. Simplifying the equations using the continuity equation and the isentropic flow assumptions
3. Solving for the Mach number at the exit of the nozzle
4. Plugging the Mach number into the equations for the pressure and velocity ratios
5. Integrating the equations to get a total pressure ratio of 5.

5. What are the applications of divergent nozzles?

Divergent nozzles have various applications in engineering, such as in rocket engines, jet engines, and steam turbines. They are also used in supersonic wind tunnels and in the design of aircraft and spacecraft. Additionally, divergent nozzles are used in industrial processes, such as in chemical reactors and waste incineration plants.

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