• Report Links
    We do not store any files or images on our server. XenPaste only index and link to content provided by other non-affiliated sites. If your copyrighted material has been posted on XenPaste or if hyperlinks to your copyrighted material are returned through our search engine and you want this material removed, you must contact the owners of such sites where the files and images are stored.
  • Home
  • -
  • New Pastes

Liquid Rocket Engine Design (Fundamentals and Calculations)

  • Thread starter King
  • Start date Nov 1, 2022

King

Administrator
Joined
Jul 12, 2021
Messages
25,005
Reaction score
5
Points
38
  • Nov 1, 2022
  • #1



Liquid Rocket Engine Design (Fundamentals and Calculations)
Published 10/2022
MP4 | Video: h264, 1280x720 | Audio: AAC, 44.1 KHz, 2 Ch
Genre: eLearning | Language: English | Duration: 18 lectures (43m) | Size: 432.7 MB


Complete guide for designing the Liquid Rocket Engine using mathematics by understanding the physics and engineering
​

What you'll learn
A lot of math computations will go into the design of the LRE. By analyzing and comprehending the engineering, you will be able to compute all the derivations.
Learn fundamentals and calculations of liquid rocket engine.
Learn how to approach the design of liquid rocket engine.
Students are capable of comprehending the fundamentals of fluid dynamics and thermodynamics.
The design of rockets can be approached mathematically by students.
Students can calculate and design liquid rocket engine CAD models.
Requirements
Basic tendency to understand the physics and engineering concepts is enough. You can learn everything about rocket engines right here.
Description
INTRODUCTION
This session will cover the thermodynamics and fluid dynamics of rocket engines and the fundamental operation of rocket engines will be addressed, along with the feed system and cooling techniques. The main topic of discussion is thermal expansion of rocket propellant.
Introduction to Liquid Rocket Engine - Propellant Choice - Feed System - Cooling Techniques - Thermal Expansion - Gas Flow in Thrust Chamber and Nozzles.
DESIGN EQUATION
We'll talk about the mathematical formulas for rocket engines in this session. The rocket nozzle's contour is calculated using equations, which is more crucial for designing a smooth flow of superheated gas inside the engine and other essential requirements.
Ejecting Velocity - Nozzle Shape Design - Nozzle Expansion Area Ratio - Combustion Chamber Design - Injector Design - Pressure...

Read more

Continue reading...
 
https://xenforo.be/
Upvote 0 Downvote
You must log in or register to reply here.
Share:
Facebook Twitter Reddit Pinterest Tumblr WhatsApp Email
  • Home
  • -
  • New Pastes
  • Terms and rules
  • Privacy policy
  • Help
  • Home
AMP generated by AMPXF.com
Menu
Log in

Register

  • Home
    • Go Premium
  • Go Premium / Advertise
  • New Ad Listings
  • What's new
    • New posts
    • New Ad Listings
    • Latest activity
  • Members
    • Registered members
    • Current visitors
X

Privacy & Transparency

We use cookies and similar technologies for the following purposes:

  • Personalized ads and content
  • Content measurement and audience insights

Do you accept cookies and these technologies?

X

Privacy & Transparency

We use cookies and similar technologies for the following purposes:

  • Personalized ads and content
  • Content measurement and audience insights

Do you accept cookies and these technologies?