962.83 KB application/pdf Download restricted. Please sign in. Restrictions Statement Barrett Honors College theses and creative projects are restricted to ASU community members. Download count: 1 Details Title Dave_H_Spring_2019.pdf Resource Type Text Part of Design and Analyze a Liquid-Liquid Swirl Coaxial Injector for a small-scale rocket engine using Computational Fluid Dynamics for minimum pressure drop and maximum spray angle. Collections this item is in Barrett, The Honors College Thesis/Creative Project Collection View full metadata Machine-readable links OAI Dublin Core MODS XML Quick actions
