Izvorni znanstveni članak

Investigation of the Pressure Distribution in a 2D Rocket Nozzle with a Mechanical System for Thrust Vector Control (TVC)

Zoran STEFANOVIĆ ; Mašinski fakultet, Univerzitet u Beogradu, Beograd, Srbija
Marko MILOŠ orcid.org/0000-0002-1931-1170 ; Mašinski fakultet, Univerzitet u Beogradu, Beograd, Srbija
Ivana TODIĆ ; Mašinski fakultet, Univerzitet u Beogradu, Beograd, Srbija
Milan PAVLOVIĆ

Sažetak

This paper introduces a new physical model of the gas flow through the 2D nozzle with the tilted obstacle in exit section. Experimental research on the 2D full span model in the supersonic indraft tunnel, which includes over three hundred tunnel runs, are presented. Variable geometric parameters were: nozzle shadow area, obstacle-nozzle wall angle, obstacle-nozzle gap and nozzle area ratio. In its conclusion, the paper discusses results and presents some suggestions for the future research.

Ključne riječi

Gas flow; Mechanical obstacle; Pressure distribution; Schlieren photo; Thrust; Thrust vector control; 2D nozzle

Hrčak ID:

80440

URI

https://hrcak.srce.hr/80440

Datum izdavanja:

31.8.2011.

Podaci na drugim jezicima: hrvatski

Posjeta: 1.256 *