نتایج جستجو برای: aerodynamic coefficients

تعداد نتایج: 115920  

2008
Mehmet SAHIN Jeremiah HALL Kamran MOHSENI Koen HILLEWAERT

Low Reynolds number aerodynamics is important for various applications including micro-aerial vehicles, sailplanes, leading edge control devices, high-altitude unmanned vehicles, wind turbines and propellers. These flows are generally characterized by the presence of laminar separation bubbles. These bubbles are generally unsteady and have a significant effect on the overall resulting aerodynam...

Journal: :IEEE Trans. Contr. Sys. Techn. 2001
Dongkyoung Chwa Jin Young Choi

This paper presents a new practical autopilot design approach to acceleration control for tail-controlled skid-to-turn (STT) missiles. The approach is novel in that the proposed parametric affine missile model adopts acceleration as the controlled output and considers the couplings between the forces as well as the moments and control fin deflections. The aerodynamic coefficients in the propose...

2009
A. N. Volkov

A three-dimensional rarefied-gas flow past a spinning sphere in the transitional and nearcontinuum flow regimes is studied numerically. The rarefaction and compressibility effects on the lateral (Magnus) force and the aerodynamic torque exerted on the sphere are investigated for the first time. The coefficients of the drag force, the Magnus force, and the aerodynamic torque are found for Mach n...

Journal: :International Journal of Aviation, Aeronautics, and Aerospace 2018

2010
M. Martinelli R. Duvigneau

This article adresses the delicate issue of estimating physical uncertainties in aerodynamics. Usually, flow simulations are performed in a fully deterministic approach, although in real life operational uncertainty arises due to unpredictable factors that alter the flow conditions. In this article, we present and compare two methods to account for uncertainty in aerodynamic simulation. Firstly...

2009
Marco Quadrelli Dhemetrios Boussalis Gregory Davis Kawai Kwok Sergio Pellegrino

The results presented in this paper apply to a generic vehicle that makes use of geometry changes to modulate the heat, drag, and acceleration loads while entering a planetary atmosphere. Two structural concepts for implementing the cone angle variation, namely a segmented shell and a corrugated shell, are presented. A structural analysis of the corrugated shell configuration shows that the str...

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