Explosive Cladding & Explosion Welding (EXW) Stand-off & Impact Calculator
Engineering preflight calculator for explosive metal cladding (EXW). Computes optimal parallel stand-off spacing, flyer impact velocity ($V_p$), collision angle ($\beta$), interfacial wavy bond wavelength, and edge exclusion scrap trim margins.
1. Input Parameters
2. Calculation Results
3. Geometric Visualizer
Tooling & Vector Prepress Engineering Notes
Explosive Cladding Physics & Jetting: Explosion welding (EXW) creates a true solid-state metallurgical bond between incompatible metals (e.g. titanium onto carbon steel) that cannot be fusion welded due to brittle intermetallic formation. The high-explosive detonation propels the flyer plate across a calibrated stand-off gap ($h_s$) at supersonic impact velocity. At the collision point, extreme pressures ($5-15\text{ GPa}$) exceed material yield strength, creating a high-velocity re-entrant metal jet that strips surface oxides ahead of the collision front.
Stand-off Gap & Edge Trim Margins: The parallel stand-off gap ($h_s \approx 0.8 - 1.5 \times t_f$) allows the flyer plate to accelerate to its terminal velocity before impacting the base plate. Along plate edges, boundary detonation rarefaction creates non-bonded or weak zones (50–120 mm), requiring generous edge trim margin exclusion lines in the final pre-cut CAM nesting vector DXFs.
Interfacial Wavy Bond Morphology: Controlled hydrodynamic flow produces a continuous interlocking wavy interface. Wavelength ($\lambda$) and amplitude ($A$) indicate bond quality and shear strength exceeding ASTM A263 / A264 / B898 standards.