Numeric study of flow separation and shock reflection hysteresis in planar nozzles.
- Published in:
- International Journal of Aerospace Innovations, 2010, v. 2, n. 4, p. 221, doi. 10.1260/1757-2258.2.4.221
- By:
- Publication type:
- Article
Works matching IS 17572258 AND DT 2010 AND VI 2 AND IP 4
Results: 6
1
2
Editorial: Underexpanded and Overexpanded Supersonic Jets.
- Published in:
- International Journal of Aerospace Innovations, 2010, v. 2, n. 4, p. i, doi. 10.1260/1757-2258.2.4.i
- By:
- Publication type:
- Article
3
Mixing Enhancement from Severely Overexpanded Nozzles.
- Published in:
- International Journal of Aerospace Innovations, 2010, v. 2, n. 4, p. 235, doi. 10.1260/1757-2258.4.4.235
- By:
- Publication type:
- Article
4
Flow Characteristics of Overexpanded Rocket Nozzles.
- Published in:
- International Journal of Aerospace Innovations, 2010, v. 2, n. 4, p. 259, doi. 10.1260/1757-2258.2.4.259
- By:
- Publication type:
- Article
5
Numerical Simulation of Overexpanded Jets in Internal and External Flows.
- Published in:
- International Journal of Aerospace Innovations, 2010, v. 2, n. 4, p. 253, doi. 10.1260/1757-2258.2.4.253
- By:
- Publication type:
- Article
6
Structure of supersonic jets with vortex generators at the nozzle exit.
- Published in:
- International Journal of Aerospace Innovations, 2010, v. 2, n. 4, p. 279, doi. 10.1260/1757-2258.2.4.279
- By:
- Publication type:
- Article