Download restricted. Restrictions Statement Barrett Honors College theses and creative projects are restricted to ASU community members. Details Title abstract.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