Date of download: 10/20/2017 Copyright © ASME. All rights reserved. From: A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber J. Turbomach. 2015;137(7):071010-071010-8. doi:10.1115/1.4029201 Figure Legend: Schematic sketch of the engine concept
Date of download: 10/20/2017 Copyright © ASME. All rights reserved. From: A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber J. Turbomach. 2015;137(7):071010-071010-8. doi:10.1115/1.4029201 Figure Legend: Meridional flow channel of the engine concept
Date of download: 10/20/2017 Copyright © ASME. All rights reserved. From: A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber J. Turbomach. 2015;137(7):071010-071010-8. doi:10.1115/1.4029201 Figure Legend: Gas generator integrated in a counter-rotating turbofan
Date of download: 10/20/2017 Copyright © ASME. All rights reserved. From: A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber J. Turbomach. 2015;137(7):071010-071010-8. doi:10.1115/1.4029201 Figure Legend: Relative Mach number and velocity vectors at 50% span for the low-speed design
Date of download: 10/20/2017 Copyright © ASME. All rights reserved. From: A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber J. Turbomach. 2015;137(7):071010-071010-8. doi:10.1115/1.4029201 Figure Legend: Combustor total pressure ratio (high-speed design) over turbine inlet temperature as a function of combustor inlet temperature for fixed Mcax3 = 0.15 and cu = 396 m/s
Date of download: 10/20/2017 Copyright © ASME. All rights reserved. From: A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber J. Turbomach. 2015;137(7):071010-071010-8. doi:10.1115/1.4029201 Figure Legend: SFC and thermal efficiency over booster stages for case 2 turbofan at test cell conditions
Date of download: 10/20/2017 Copyright © ASME. All rights reserved. From: A Novel Gas Generator Concept for Jet Engines Using a Rotating Combustion Chamber J. Turbomach. 2015;137(7):071010-071010-8. doi:10.1115/1.4029201 Figure Legend: Thermal efficiency of case I (conventional turbofan), case II (low-speed gas generator turbofan), and case III (high-speed gas generator turbofan), at test cell conditions