Method of calculating the longitudinal, lateral, and crossed aerodynamic derivatives of an aircraft at subsonic velocities

DOI10.1007/BF01091671zbMath0448.76050OpenAlexW2040415806MaRDI QIDQ1147042

F. I. Ganiev

Publication date: 1978

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01091671

zbMATH Keywords

computation methodlongitudinal, lateral and cross aerodynamical derivativeswinged aircraft

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Numerical differentiation (65D25) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Cites Work

• Proof of the numerical method of 'discrete vortices' for solving singular integral equations

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