3D-model of compressor rotor blade development

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

Russian Federation

student

A. I. Ryazanov

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Email: tr05@bk.ru

Russian Federation

junior member

L. A. Chempinsky

Samara State Aerospace University named after academician S.P. Korolyov (National Research University)

Email: chempinskiy@mail.ru

Russian Federation

candidate of technical sciences
professor of «Aircraft engines manufacturing» department

References

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