Optimization of forming parameters for fiberglass shells of rocket nose cones by a criticality criterion

Optimization of forming parameters for fiberglass shells of rocket nose cones by a criticality criterion

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 coni...

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Veröffentlicht in:Russian aeronautics 2017, Vol.60 (1), p.141-149
Hauptverfasser: Urazbakhtin, F. A., Kharinova, Yu. Yu, Urazbakhtina, A. Yu
Format: Artikel
Sprache:eng
Schlagworte:
Aircraft Production Technology
Automotive Engineering
Criteria
Engineering
Fiberglass
Forming
Nose cones
Parameters
Rocket nose cones
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Beschreibung
Zusammenfassung: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.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799817010214