THEORETICAL PREDICTION OF PRESSURES IN HYPERSONIC FLOW WITH SPECIAL REFERENCE TO CONFIGURATIONS HAVING ATTACHED LEADING-EDGE SHOCK Part Ⅰ. Theoretical Investigation

摘要

An investigation has been undertaken to develop theories for predicting pressures in hypersonic flows, with special reference to low-aspect-ratio, delta-winged configurations. This report is the first of four covering our work to data and is concerned primarily with the following theoretical developments which, for the most part, are directed at the treatment of sharp-leading-edge shapes.