Publisher
American Institute of Aeronautics and Astronautics
Reference9 articles.
1. Paxson, D.E. and Dougherty, K.T., 2005, `Ejector enhanced pulsejet based pressure gain combustors: An old idea with a new twist',NASA/TM-2005-213854AIAA-2005-4216
2. Porter,C.D.,1958,`Valveless-gas-turbinecombustorswithpressuregain',ASMEPaperNo.58-GTP-11,pp.179-184
3. Performance of Choked Unsteady Ejector-Nozzles for use in Pressure Gain Combustors
4. Convective Heat Transfer and Aerodynamics in Axial Flow Turbines