Part I is an introduction to an empirical and theoretical study of two-dimensional aerofoil flows which include a limited region of supersonic flow terminated by a shock wave. A brief review of theoretical studies of the ...
Flight measurements made by Mair in 1942, with the wake-traverse method, are used to extend to high Reynolds numbers (2 x 107) and a thick section (18 per cent t/c) the verification that the sub-critical creep (slow increase ...