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3D-model of compressor rotor blade development
- Authors: Boyarov K.V.1, Ryazanov A.I.1, Chempinsky L.A.1
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Affiliations:
- Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
- Issue: Vol 10, No 3-3 (2011): Special Issue
- Pages: 182-190
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6878
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-3(27)-182-190
- ID: 6878
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Abstract
3D-model of compressor rotor blade is developed. Structural elements of the model: comprehensive representative of dovetail shank type and blade airfoil are parametrized.
About the authors
K. V. Boyarov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Author for correspondence.
Email: konst90@gmail.com
student
Russian FederationA. I. Ryazanov
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: tr05@bk.ru
junior member
Russian FederationL. A. Chempinsky
Samara State Aerospace University named after academician S.P. Korolyov (National Research University)
Email: chempinskiy@mail.ru
candidate of technical sciences
professor of «Aircraft engines manufacturing» department
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