Numerical Simulation of a Two-Dimensional Spatial Unsteady Flow Past Thick Airfoils and Low-Aspect-Ratio Wings with Slot Suction in a Vortex Cell as Applied to Hybrid Aerostatic Aircraft
Crossref DOI link: https://doi.org/10.1007/s10891-023-02736-7
Published Online: 2023-06-24
Published Print: 2023-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Isaev, S. A.
Usachov, A. E.
Sustin, S. A.
Nikushchenko, D. V.
Sudakov, A. G.
Tryaskin, N. V.
Text and Data Mining valid from 2023-05-01
Version of Record valid from 2023-05-01
Article History
Received: 2 March 2022
First Online: 24 June 2023