Courses

    Focuses on the applications of the first and second laws of thermodynamics to control volumes and teaches the fundamental concepts of different modes of energy and heat transfer. Learn to use these concepts in gas dynamics, high-speed vehicle spacecraft design, environmental systems, and energy analysis. Offered fall only. Prerequisites: Requires prerequisite courses of ASEN 2002 and APPM 2350 or MATH 2400 (all minimum grade C). Restricted to Aerospace Engineering (ASEN) majors only.
    Describes aerothermodynamics and design of both rocket and air-breathing engines. Includes ramjets, turbojets, turbofans, and turboprop engines, as well as liquid, solid, and hybrid rockets. Prerequisites: Requires prerequisite courses of ASEN 3113 and APPM 2360 (all minimum grade C). Restricted to Aerospace Engineering (ASEN) or Aerospace Engineering Concurrent Degree (C-ASEN) majors only.
    An in depth presentation of the theory, analysis, and design of rocket propulsion systems. Liquid and solid propellant systems are emphasized with an introduction to advanced propulsion concepts. Nozzle and fluid flow relationships are reviewed for background. Prerequisites: Restricted to College of Engineering (ENGR) graduate students or Aerospace Engineering Concurrent Degree (C-ASEN) majors only.
    Designed to teach the theory, analysis and design of modern gas turbine engines used for aircraft propulsion. Will deal with cycle and performance analyses, and analysis and design of compressors, turbines, intakes, nozzles and combustors as well as component matching. Recommended prereq., ASEN 4013 or equivalent or instructor consent required. Prerequisites: Restricted to College of Engineering (ENGR) graduate students or Aerospace Engineering Concurrent Degree (C-ASEN) majors only.
    Covers air-breathing and rocket propulsion cycles, their relative performance trade-offs, and how they fit within the context of a vehicle system. Specific emphasis will be placed on fundamental cycle analyses, component level design, and propulsion/airframe integration for rockets, turbojets, ramjets, scramjets, combined cycles, and other advanced propulsion concepts. Recommended prereq., ASEN 4013 or equivalent or instructor consent required. Prerequisites: Restricted to College of Engineering (ENGR) graduate students or Aerospace Engineering Concurrent Degree (C-ASEN) majors only.