Final report on effects of Reynolds number on unsteady flow response of NACA 0020 aerofoil : carried out at University College London.
Energy Technology Support Unit (Great Britain)
University College, London.
[London] : [University College],
1988.
Work described in this report was performed under contract for ETSU on behalf of the Department of Energy.
Contract no.E/5A/CON/5075/1569.
Aerofoils.
Air-turbines