Abstract
A computational platform of a supersonic inlet with variable geometry was devewped using MATLAB/SIMU-LINK. A method based on the platform for simulation of a complicated model has been presented. The correctness and reliability of the new method have been testified by simulating the stationary flow fields of an inlet under back pressure vibration and vibration parameters of incoming air flow. Based on the method, the dynamic behavior of the terminal normal shock wave in the inlet has been obtained by carrying out a simulation of the object model of an inlet, and the dynamic and stationary characteristics have also been obtained. A complicated distributed parameter problem of an one-dimensional supersonic inlet has been transformed to a zero dimensional problem which overcomes concentrative-parameter difficulty.
| Original language | English |
|---|---|
| Pages (from-to) | 199-203 |
| Number of pages | 5 |
| Journal | Tuijin Jishu/Journal of Propulsion Technology |
| Volume | 28 |
| Issue number | 2 |
| State | Published - May 2007 |
Keywords
- Dynamic simulation
- Normal shock wave
- Starting
- Supersonic inlet
Fingerprint
Dive into the research topics of 'A simulation method based on SIMULINK for a supersonic inlet'. Together they form a unique fingerprint.Cite this
- APA
- Author
- BIBTEX
- Harvard
- Standard
- RIS
- Vancouver