Experiments and analysis for a gust generator in a wind tunnel

Deman Tang, Paul G. A. Cizmas, Earl H. Dowell

Journal of Aircraft · 1996 · 80 citations · 4 references

Concepts

TL;DR

The gust generator uses a rotating slotted cylinder in a low‑speed wind tunnel, offering a simple, low‑cost design that can produce controllable single or multiple harmonic gusts with minimal power and torque. The study proposes a simplified theoretical aerodynamic model and design estimation for the lateral and longitudinal gust flowfield. The authors performed an experimental investigation of the gust field from a rotating slotted cylinder and developed a design estimate based on a two‑dimensional dynamic lift coefficient derived from theoretical and experimental data. The primary drawback identified is an interfering wake vortex effect. Nomenclature definitions for variables such as C(k), ICleql, c, d, dLa, dLrsc, e, elc, H, HIHW, and Hw are provided.

Abstract

An experimental investigation was made of the gust field generated by a rotating slotted cylinder installed in the Duke University low-speed, closed-circuit wind tunnel. The system has a very simple configuration with low cost and can produce a controllable single or multiple harmonic gust wave in the lateral and longitudinal directions. It requires minimal power and torque input. A simplified theoretical aerodynamic model and a design estimation of the lateral and longitudinal gust flowfield is also proposed in this article. The design estimate is based on a two-dimensional dynamic lift coefficient that is given by the theoretical and experimental results. An interfering wake vortex effect is the major disadvantage of this system. Nomenclature C(k) = Theodorsen's function ICleql = magnitude of equivalent lift coefficient for rotating slotted cylinder/airfoil c = airfoil chord d = cylinder diameter dLa = airfoil lift force per span length dLrsc = rotating slotted cylinder lift force per span length e, e = gap between the o.d. of the rotating slotted cylinder and trailing edge of the airfoil, elc H, H = vertical position from tunnel bottom, HIHW Hw = height of the tunnel test section

References

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