115.01 KB application/pdf Download restricted. Please sign in. 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