The Lift on a Wing in a Turbulent Flow
- 1 August 1973
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 24 (3), 155-166
- https://doi.org/10.1017/s0001925900006569
Abstract
Summary Experiments are described in which the lift on a rectangular element of a two-dimensional wing and on a finite aspect ratio wing has been measured in grid turbulence. By measuring the spectrum of the lift and the spectrum of the turbulence upwash component, an experimental value for the turbulent admittance may be found. This is compared with a calculated value based upon linearised theory.Keywords
This publication has 7 references indexed in Scilit:
- A Lifting-Surface Theory for the Rectangular Wing in Non-Stationary FlowAeronautical Quarterly, 1971
- Lifting Surface Theory for the Problem of an Arbitrarily Yawed Sinusoidal Gust Incident on a Thin Aerofoil in Incompressible FlowAeronautical Quarterly, 1970
- Spectral Theory of Buffeting and Gust Response: Unification and ExtensionJournal of the Aeronautical Sciences, 1956
- Extension of the Statistical Approach to Buffeting and Gust Response of Wings of Finite SpanJournal of the Aeronautical Sciences, 1955
- On the Application of Statistical Concepts to the Buffeting ProblemJournal of the Aeronautical Sciences, 1952
- Some Aspects of Non-Stationary Airfoil Theory and Its Practical ApplicationJournal of the Aeronautical Sciences, 1941
- Airfoil Theory for Non-Uniform MotionJournal of the Aeronautical Sciences, 1938