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Journal ArticleDOI

Approximate transfer functions for large aspect ratio wings in turbulent flow

L. T. Filotas
- 01 Jun 1971 - 
- Vol. 8, Iss: 6, pp 395-400
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TLDR
In this article, the authors derived approximate closed form expressions for the gust transfer functions relating the lift and moments to the upwash in such a wave, and suggested simple scaling laws, based on these results, are then suggested for flight through large scale turbulence.
Abstract
The fundamental aerodynamic problem associated with flight through atmospheric turbulence is calculation of the response of a wing flying through a single sinusoidal wave of upwash with lines of constant phase arbitrarily inclined to the flight path. Approximate closed form expressions for the gust transfer functions" relating the lift and moments to the upwash in such a wave are derived for large aspect ratio rectangular wings in incompressible flow. The lift transfer function is expressed as the usual two-dimensional Sears function multiplied by a factor to correct for finite span and a further factor to account for the span wise gust wave number. Multiplying this expression by the chordwise (or spanwise) center of pressure leads to the pitching (or rolling) moment transfer function. Some simple scaling laws, based on these results, are then suggested for flight through large-scale turbulence.

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Citations
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Turbulent Wind and Its Effect on Flight

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Rotating blades and aerodynamic sound

TL;DR: The history of research on rotating blade noise is reviewed in this paper, from early studies of propeller radiation to current work on aircraft-engine fans, with emphasis on fundamental aspects of aerodynamic sound generation by blades.
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Aerodynamic Effects on Wind Turbulence Measurements with Research Aircraft

TL;DR: In this paper, the effects of the propellers of a turboprop aircraft and of the aircraft vortex system on the pressure and wind velocity measurements near the nose of an aircraft are examined.
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Wind Modeling and Lateral Control for Automatic Landing

TL;DR: In this paper, a lateral control system for the automatic landing of a DC-8 aircraft is presented. But the authors do not consider the effect of crosswind shear and turbulence on the aircraft aerodynamic forces.
Journal ArticleDOI

Direct measurement of the Sears function in turbulent flow

TL;DR: In this article, the applicability of the strip assumption in the estimation of the unsteady lift response of a two-dimensional wing in turbulent flow is investigated, where the ratio between the lift spectrum calculated from the two-wavenumber analysis and the estimate from the strip assumptions is used to evaluate the accuracy of the estimate.
References
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Book

A treatise on the theory of Bessel functions

G. N. Watson
TL;DR: The tabulation of Bessel functions can be found in this paper, where the authors present a comprehensive survey of the Bessel coefficients before and after 1826, as well as their extensions.
Journal ArticleDOI

Some Aspects of Non-Stationary Airfoil Theory and Its Practical Application

TL;DR: In this paper, the lift and moment of a rigid airfoil passing through a vertical-gust pattern having a sinusoidal distribution of intensity were derived for two-dimensional thin airfoils in non-uniform motion.
Book

Dynamics of flight

Etkin Bernard