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: 20 dec. 2024. 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
%A Martinis, Vinko %A Matijašević, Branimir %A Tuković, Željko %D 2002 %T A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design %B 2002 %9 supersonic nozzle; nozzle design; numerical solutions; inverse problems; %! 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 %P 8 %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. 20 Dec. 2024
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/
@article{{}{.}, 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}, doi = {}, url = {https://www.sv-jme.eu/sl/article/a-numerical-solution-to-the-inverse-problem-of-supersonicnozzle-design/} }
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)
Strojniški vestnik - Journal of Mechanical Engineering 48(2002)4, 210-217
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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.