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

DOI10.1134/S0015462813020142zbMath1269.76053MaRDI QIDQ359316

Publication date: 9 August 2013

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

aerodynamic derivatives delta wing harmonic oscillations high angles of attack mathematical model of aerodynamic forces reduced oscillation frequency

Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05) General aerodynamics and subsonic flows (76G25)

Cites Work

Mathematical description of nonstationary aerodynamic characteristics of a passenger aircraft model in longitudinal motion at large angles of attack

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