Optimization of forming parameters for fiberglass shells of rocket nose cones by a criticality criterion
- Authors: Urazbakhtin F.A.1, Kharinova Y.Y.1, Urazbakhtina A.Y.1
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Affiliations:
- Kalashnikov Izhevsk State Technical University, Votkinsk Branch
- Issue: Vol 60, No 1 (2017)
- Pages: 141-149
- Section: Aircraft Production Technology
- URL: https://journal-vniispk.ru/1068-7998/article/view/230039
- DOI: https://doi.org/10.3103/S1068799817010214
- ID: 230039
Cite item
Abstract
Forming of fiberglass shells by a winding method for the purpose of detecting the criticalities is analyzed. The quantitative assessments of criticalities are introduced as a finite set of indexes that are the multipurpose criticality functions. The optimal parameters for forming the fiberglass conic shell are found with respect to the criticality criterion.
About the authors
F. A. Urazbakhtin
Kalashnikov Izhevsk State Technical University, Votkinsk Branch
Author for correspondence.
Email: uras_51@mail.ru
Russian Federation, ul. Shuvalova 1, Votkinsk, 427430
Yu. Yu. Kharinova
Kalashnikov Izhevsk State Technical University, Votkinsk Branch
Email: uras_51@mail.ru
Russian Federation, ul. Shuvalova 1, Votkinsk, 427430
A. Yu. Urazbakhtina
Kalashnikov Izhevsk State Technical University, Votkinsk Branch
Email: uras_51@mail.ru
Russian Federation, ul. Shuvalova 1, Votkinsk, 427430
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