A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design

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Izvoz citacije: ABNT
MARTINIS, Vinko ;MATIJAŠEVIĆ, Branimir ;TUKOVIĆ, Željko .
A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design. 
Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 48, n.4, p. 210-217, november 2017. 
ISSN 0039-2480.
Available at: <https://www.sv-jme.eu/sl/article/a-numerical-solution-to-the-inverse-problem-of-supersonicnozzle-design/>. Date accessed: 11 nov. 2019. 
doi:http://dx.doi.org/.
Martinis, V., Matijašević, B., & Tuković, .
(2002).
A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design.
Strojniški vestnik - Journal of Mechanical Engineering, 48(4), 210-217.
doi:http://dx.doi.org/
@article{.,
	author = {Vinko  Martinis and Branimir  Matijašević and Željko  Tuković},
	title = {A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {48},
	number = {4},
	year = {2002},
	keywords = {supersonic nozzle; nozzle design; numerical solutions; inverse problems; },
	abstract = {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.},
	issn = {0039-2480},	pages = {210-217},	doi = {},
	url = {https://www.sv-jme.eu/sl/article/a-numerical-solution-to-the-inverse-problem-of-supersonicnozzle-design/}
}
Martinis, V.,Matijašević, B.,Tuković, .
2002 November 48. A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 48:4
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%A Matijašević, Branimir 
%A Tuković, Željko 
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%! A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design
%K supersonic nozzle; nozzle design; numerical solutions; inverse problems; 
%X 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.
%U https://www.sv-jme.eu/sl/article/a-numerical-solution-to-the-inverse-problem-of-supersonicnozzle-design/
%0 Journal Article
%R 
%& 210
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%J Strojniški vestnik - Journal of Mechanical Engineering
%V 48
%N 4
%@ 0039-2480
%8 2017-11-06
%7 2017-11-06
Martinis, Vinko, Branimir  Matijašević, & Željko  Tuković.
"A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design." Strojniški vestnik - Journal of Mechanical Engineering [Online], 48.4 (2002): 210-217. Web.  11 Nov. 2019
TY  - JOUR
AU  - Martinis, Vinko 
AU  - Matijašević, Branimir 
AU  - Tuković, Željko 
PY  - 2002
TI  - A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design
JF  - Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - supersonic nozzle; nozzle design; numerical solutions; inverse problems; 
N2  - 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.
UR  - https://www.sv-jme.eu/sl/article/a-numerical-solution-to-the-inverse-problem-of-supersonicnozzle-design/
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	author = {Martinis, V., Matijašević, B., Tuković, .},
	title = {A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {48},
	number = {4},
	year = {2002},
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TY  - JOUR
AU  - Martinis, Vinko 
AU  - Matijašević, Branimir 
AU  - Tuković, Željko 
PY  - 2017/11/06
TI  - A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design
JF  - Strojniški vestnik - Journal of Mechanical Engineering; Vol 48, No 4 (2002): Strojniški vestnik - Journal of Mechanical Engineering
DO  - 
KW  - supersonic nozzle, nozzle design, numerical solutions, inverse problems, 
N2  - 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.
UR  - https://www.sv-jme.eu/sl/article/a-numerical-solution-to-the-inverse-problem-of-supersonicnozzle-design/
Martinis, Vinko, Matijašević, Branimir, AND Tuković, Željko.
"A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 48 Number 4 (06 November 2017)

Avtorji

Inštitucije

  • University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Croatia
  • University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Croatia
  • University of Zagreb, Faculty of Mechanical Engineering and Naval Architecture, Croatia

Informacije o papirju

Strojniški vestnik - Journal of Mechanical Engineering 48(2002)4, 210-217

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.

supersonic nozzle; nozzle design; numerical solutions; inverse problems;