NASA NTRS · 19690050298
Stress waves resulting from hypervelocity impact.
Abstract
Characteristics method for stress waves from hypervelocity impact of circular cylinder on half space, discussing numerical diffusion effect on pressure and flow fields
Keep this discovery
Explore connections, maps & timelines
Chang, T. S., Madden, R.. 1969-04-01. Stress waves resulting from hypervelocity impact.. https://ntrs.nasa.gov/citations/19690050298
Cite the original work for its findings. Save a collection to share your selection of sources.