GrabCAD 模型信息
Converging Diverging Rocket Nozzle (Request 2 redux) · 模型 209358
This is a re-design of the CD rocket nozzle originally posted here: https://grabcad.com/library/rocket-nozzle-request-2-1 I redesigned the nozzle in SolidWorks and exported the files as STLs for use in CFD software. The nozzle has an Ae/A*= 14.06 and Ai/A*=1.602. I've also included STL surfaces of the inlet and outlet for CFD purposes.
- 格式
- STL、STEP / IGES、SOLIDWORKS、Parasolid
- 分类
- Aerospace、Aviation、Components
- 标签
- stl、cd、nozzle、rocket
- 数据更新
- 2026-10-26T08:55:21Z
