Design method of three-dimensional internal rotating four-channel hypersonic speed combination air inlet channel
The invention discloses a design method of a three-dimensional internal rotating four-channel hypersonic speed combination air inlet channel. The design method comprises the steps that a punching channel with the working Mach number range Ma being 4 to 6 is designed; an ejection rocket channel flow-...
Gespeichert in:
| Hauptverfasser: | , , , |
|---|---|
| Format: | Patent |
| Sprache: | chi ; eng |
| Schlagworte: | |
| Online-Zugang: | Volltext bestellen |
| Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
| Zusammenfassung: | The invention discloses a design method of a three-dimensional internal rotating four-channel hypersonic speed combination air inlet channel. The design method comprises the steps that a punching channel with the working Mach number range Ma being 4 to 6 is designed; an ejection rocket channel flow-dividing plate and a turbine channel flow-dividing plate are designed, airflow entering an ejectionrocket channel and a turbine channel is rotationally adjusted through the flow-dividing plates, and the flow-dividing plates are designed by combining the layout of the ejection rocket channel and theturbine channel; a turbine channel expansion section with the working Mach number range Ma being 0 to 2 is designed; and an ejection rocket channel expansion section with the working Mach number range Ma being 2 to 4 is designed. The three-dimensional internal rotating four-channel hypersonic speed combination air inlet channel comprises a three-dimensional internal rotating air inlet channel compression profile, a punchi |
|---|