Computer Code For 3-D Rocket Thermal Evaluation

In summary, a user shared a link to a user manual for RTE2002, a computer code for three-dimensional rocket thermal evaluation. The manual also includes other papers in pdf format. The user expresses their interest in rocket technology and the usefulness of having access to such codes.
  • #1
Astronuc
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Stumbled across this and thougth folks around here might find it of interest and perhaps even useful.

USER MANUAL FOR RTE2002
Version 1
A COMPUTER CODE FOR THREE-DIMENSIONAL
ROCKET THERMAL EVALUATION

http://home.manhattan.edu/~mohammad.naraghi//rte/rte.pdf

Page with several other papers in pdf format
http://home.manhattan.edu/~mohammad.naraghi//rte/rte.html
 
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  • #2
Well, seems it is a lot of work done.

But as my current status reveals that I'm devoted to Science at least so far, I don't like that code. I am not particularly friend of correlations. Also, with exception of the solution of the heat equation inside the wall, there is no mathematical robustness, and I haven't seen what is going on with the flow field which turns out to have a capital importance in the heat transfer. The only thing that I see is modelling the flow are those horrible correlations.
 
  • #3


Wow, thanks for sharing this resource! As someone interested in rocket technology, I'll definitely be checking out this user manual for RTE2002. It's always useful to have access to computer codes for thermal evaluation, especially when it comes to three-dimensional applications. And the fact that there are other papers available in pdf format on the same page is a great bonus. Thanks again for sharing!
 

FAQ: Computer Code For 3-D Rocket Thermal Evaluation

What is "Computer Code For 3-D Rocket Thermal Evaluation"?

"Computer Code For 3-D Rocket Thermal Evaluation" is a software program used to simulate and analyze the thermal behavior of a 3-D rocket during launch and flight. It takes into account factors such as heat transfer, material properties, and environmental conditions to accurately predict the temperature distribution of the rocket and its components.

How does the code work?

The code uses mathematical equations and advanced algorithms to model the heat transfer and thermal behavior of the rocket. It takes into account the geometry and material properties of the rocket, as well as external factors such as air temperature and pressure. The code then runs simulations to predict the temperature distribution and any potential hot spots on the rocket.

What are the benefits of using this code?

The code allows for more accurate and efficient thermal analysis of a 3-D rocket, which is crucial for ensuring the safety and success of a launch. It can also help engineers optimize the design of the rocket to withstand high temperatures and reduce the risk of thermal damage.

Is the code customizable?

Yes, the code can be customized to fit the specific needs and requirements of a particular rocket design. This includes adjusting parameters and inputs, as well as incorporating different materials and environmental conditions.

Who can use this code?

This code can be used by engineers, researchers, and scientists working in the field of rocket design and development. It requires a strong understanding of thermal dynamics and programming skills to effectively use and interpret the results from the code.

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