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Ways 3D parametrization TJ blades for use CAD/CAM/CAE packages
- Authors: Smelov V.G.1, Shitarev I.L.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 7, No 3 (2008): Special Issue
- Pages: 44-47
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/608
- DOI: https://doi.org/10.18287/2541-7533-2008-0-3(16)-44-47
- ID: 608
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Abstract
Article is devoted to an actual problem of modern aviation propulsion engineering - to creation of parametrical model blades. In article results of work on parametrization blades the compressor of 7 steps of engine NK 14 ST are resulted. The program on creation macros for formation 3D is submitted to model to a feather blades. Areas of use of results of work are discussed.
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About the authors
V. G. Smelov
Samara State Aerospace University
Author for correspondence.
Email: pdla_smelov@mail.ru
Russian Federation
I. L. Shitarev
Samara State Aerospace University
Email: pdla_smelov@mail.ru
Russian Federation
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