A. Savelyev

发表

Allowance for Gas Compressibility in the γ-Model of the Laminar–Turbulent Transition

E. Matyash, A. Savelyev, A. Troshin, 2019, Computational Mathematics and Mathematical Physics.

Optimal design and installation of ultra high bypass ratio turbofan nacelle

Andrey Vladimirovich Shenkin, S. V. Mikhaylov, Nikolay Alekseevich Zlenko, 2016 .

Enhancing optimization capabilities using the AGILE collaborative MDO framework with application to wing and nacelle design

Pier Davide Ciampa, Fabrizio Nicolosi, Nathalie Bartoli, 2020 .

Robust Nacelle Optimization Design investigated in the AGILE European project

Nathalie Bartoli, Thierry Lefebvre, Kirill Anisimov, 2018, 2018 Multidisciplinary Analysis and Optimization Conference.

Computational study of engine external aerodynamics as a part of multidisciplinary optimization procedure

Kirill Anisimov, Andrey Savelyev, Innocentiy A. Kursakov, 2016 .

METHOD OF OPTIMAL AERODYNAMIC DESIGN OF THE NACELLE FOR THE MAIN PROPULSION SYSTEM WITH A HIGH BYPASS RATIO

Andrey Vladimirovich Shenkin, S. V. Mikhaylov, Nikolay Alekseevich Zlenko, 2015 .

Uncertainty quantification and robust design optimization applied to aircraft propulsion systems

Artur Mirzoyan, Kirill Anisimov, Andrey Savelyev, 2018 .

Collaborative System of Systems Multidisciplinary Design Optimization for Civil Aircraft: AGILE EU project

Luca Boggero, Marco Fioriti, Artur Mirzoyan, 2017 .

Design of the Strut Braced Wing Aircraft in the AGILE Collaborative MDO Framework

Marco Fioriti, Francesca Tomasella, Pier Davide Ciampa, 2018 .

CFD simulations of the flow control performance applied for inlet of low drag high-bypass turbofan engine at cross flow regimes

E. V. Kazhan, A. V. Lysenkov, I. A. Kursakov, 2016 .

AERODYNAMIC OPTIMIZATION OF AIRPLANE PROPULSION SYSTEM WITHIN THE FRAMEWORK OF AGILE PROJECT

K. S. Anisimov, A. Savelyev, K. Anisimov, 2016 .