Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 3: Some Applications of Oscillating Lifting Surface Theory to the Flapping Wing

INCAS Bulletin

Valentin Adrian Jean BUTOESCU¹ 

[1] INCAS – National Institute for Aerospace Research “Elie Carafoli” B-dul Iuliu Maniu 220, Bucharest 061126, Romania [e-mail];

关键词: Lifting surface;    integral equation;    harmonic oscillations;    generalised airforces;    flutter;    flapping wings;    Fourier series;    Fourier transform;   

DOI  :  10.13111/2066-8201.2014.6.2.2

来源: DOAJ

【 摘 要 】

The third article of this series continues to deal with the calculation of the aerodynamic unsteady forces on lifting surfaces. Here we present how the theory of oscillating wing in subsonic flow can be applied to the aerodynamic response to certain kinds of wing motions or gusts.

【 授权许可】

Unknown