Aerospace Engineering Department
BS in Aerospace Engineering
A ramjet combustion chamber is designed and some initial assembly fabrication and test completed as a component of a ramjet graduate project for California Polytechnic State University, San Luis Obispo Supersonic Wind Tunnel. The combustor design is driven by a theoretical model created by a Cal Poly graduate student, Harrison Sykes. Temperature, pressure, and fuel flow will be measured.
Aerodynamics and Fluid Mechanics Commons, Aeronautical Vehicles Commons, Fluid Dynamics Commons, Heat Transfer, Combustion Commons, Other Aerospace Engineering Commons, Propulsion and Power Commons, Thermodynamics Commons