The numerical design of a nozzle is sensitive to stability in the region of supersonic flow. In the numerical algorithm presented in this paper the instability is avoided by the introduction of an analytically set pressure distribution on the axis of the axisymmetrical supersonic nozzle. The flow parameters of the inverse designed nozzle are checked by the application code FLUENT and they show a regular distribution on cross-sections along the nozzle.

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URN

URN:NBN:SI:DOC-JVYLM51S

COBISSID

5392155

Added

16.09.2009

Metadata

Citation

APA:

Martinis, Vinko, Matijašević, Branimir, Tuković, Željko (2002). Računsko reševanje inverznega problema oblikovanja nadzvočne šobe. Strojniški vestnik, volume 48, issue 4, str. 210-217. URN:NBN:SI:DOC-JVYLM51S from http://www.dlib.si

MLA:

Martinis, Vinko, Matijašević, Branimir, Tuković, Željko. "Računsko reševanje inverznega problema oblikovanja nadzvočne šobe." Strojniški vestnik volume 48. issue 4 (2002) str. 210-217.
<http://www.dlib.si/?URN=URN:NBN:SI:DOC-JVYLM51S>

Strojniški vestnik
1955-
(Assembly record)

številka

Strojniški vestnik
2002
(Complete issue)

Računsko reševanje inverznega problema oblikovanja nadzvočne šobeA numerical solution in the inverse problem of supersonic-nozzle design

Računsko reševanje inverznega problema oblikovanja nadzvočne šobe
A numerical solution in the inverse problem of supersonic-nozzle design