Recent Assessment and Analysis of Damping Derivatives for Delta Wings in Hypersonic Flow for Curved Leading Edges with Full Sine Wave
Because of the pitch rate for the different amplitude of the sinus wave, flow deflection angle δ, pivot position, and the Mach numbers, this paper presents the influence of curved leading edges on the damping derivative. Results show that there is a gradual rise in the pitch damping derivatives from h = 0 with the…
Read more