ESDU AERO W.01.01.05
Slope of lift curve for two-dimensional flow.
Abstract:ESDU AERO W.01.01.05 is retained in the Series because it is referred to and used in a number of ESDU documents in Aerodynamics. To obtain values of the slope of the lift coefficient curve with angle of attack on an aerofoil in incompressible (or compressible but subcritical) flow, ESDU 72024 and ESDU 97020 should be used.
|Data Item ESDU AERO W.01.01.05|
The graphs listed below are available only to subscribers.
|Figure 1||(a1)0 / (a1)0T for leading-edge transition|
|Figure 2||(a1)0 / (a1)0T for mid-chord transition|
|Figure 3||Theoretical lift-curve slope|
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