High-Range Delta-Winged Hypersonic Projectile Concept for Low-Cost Production
Mary Zoeller et al.
This study presents a delta wing body for the UCAH Undergraduate Hypersonic Flight Design Competition, optimized for maximum low altitude range while meeting strict requirements on Mach number, stability, thermal survivability, size, mass, and maneuver capability. The configuration blends a blunted diamond nose with a moderately swept delta planform to harness vortex lift, preserve internal volume for structure and controls, and manage aeroheating through appropriate leading edge radius and skin