A Vortex-Lattice Method for Calculating Longitudinal Dynamic Stability Derivatives of Oscillating Delta Wings

DOI10.2514/3.48413zbMATH Open0533.73047OpenAlexW2002903350MaRDI QIDQ3316710

No author found.

Publication date: 1984

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.48413

zbMATH Keywords

delta wingoscillatory motiondynamic stability derivativesnonsteady vortex-lattice methodresults for damping in pitchsmall oscillations in pitch

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Theory of constitutive functions in solid mechanics (74A20) Numerical and other methods in solid mechanics (74S99)

Related Items (1)

Aerodynamic characteristics of a deltawing in the case of harmonic oscillations with respect to the roll and yaw angles at high angles of attack

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