Calculated velocity distributions and force derivatives for a series of high-speed aerofoils / by C.S. Sinnott.
L.C. Woods' Polygon method is used to calculate the velocity distribution over a number of two-dimensional aerofoils at low incidence, subcritical flows only being considered. Lift slopes and aerodynamic centers at zero lift are also calculated.
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| Format: | Book |
| Language: | English |
| Published: |
London :
H.M.S.O,
1957.
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| Series: | Reports and memoranda (Aeronautical Research Council (Great Britain)) ;
no. 3045. |
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