powerpoint presentation...three keys to reducing supersonic i-to noise engines: sufficient thrust...

10

Upload: others

Post on 02-Aug-2020

1 views

Category:

Documents


0 download

TRANSCRIPT

Page 1: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 2: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 3: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 4: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 5: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 6: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 7: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 8: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 9: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise
Page 10: PowerPoint Presentation...Three keys to reducing supersonic I-TO noise Engines: sufficient thrust while constrained on fan size and takeoff jet velocity Aerodynamics: adequate cruise