1. 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): doi: /
Figure Legend:
Schematic sketch of the engine concept

2. 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): doi: /
Figure Legend:
Meridional flow channel of the engine concept

3. 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): doi: /
Figure Legend:
Gas generator integrated in a counter-rotating turbofan

4. 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): doi: /
Figure Legend:
Relative Mach number and velocity vectors at 50% span for the low-speed design

5. 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): doi: /
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

6. 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): doi: /
Figure Legend:
SFC and thermal efficiency over booster stages for case 2 turbofan at test cell conditions

7. 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): doi: /
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