Global ETD Search
Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.
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Showing 1 to 3 of 3 for “"Rocket Propulsion System"”.
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Development, modeling and testing of a slow-burning solid rocket propulsion system
… are expanding the capabilities of aircraft systems. However, a gap exists in the size and capability of aircraft: no aircraft smaller than 10 kilograms are capable of flight faster than 100 meters per second. A small, fast aircraft requires a propulsion system which is both miniature and …
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Increased confidence in concept design through trade space exploration and multiobjective optimization
… size, complexity and demands of engineering systems requires paying greater attention to the initial design of the system concept. To improve the process by which concept design is carried out, this thesis develops an Engineering Framework for Concept Development. The Engineering Framework is …
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Numerical Simulations of Multi-Confined Jets in Crossflow at Supercritical Pressure
… applications such as in gas turbine film cooling system, fuel atomization for scramjet engine, vertical takeoff and landing of an aircraft, and core fluid of liquid rocket engine pre-burner. The Reynolds Averaged Navier Stokes (RANS) equations were solved using k-ε and k-ꞷ turbulence models for …