Bolton Shaw, B. W.2012-06-082012-06-081950-05http://dspace.lib.cranfield.ac.uk/handle/1826/7206Expressions are derived for lξ and a2 of nose ailerons and nose elevators on a delta wing, as depicted in Fig. 1, in supersonic flight. Nose and trailing edge controls on delta wings in supersonic flight are compared.enReport