E. W. E. Rogers; J. L. Attridge; Miss A. G. J. Macdonald; J. Callinan
(1964)
Tests have been made at a Mach number of 4.03 and Reynolds number of 3.4 million on two families of models, consisting of delta wings with underslung half-Cone bodies. The wing sweepback angles were 75° and 80°, and the ...