Three proposed SCAR propulsion systems in terms of aircraft range for a fixed payload and take-off gross weight with a design cruise Mach number 2.7 are evaluated. The effects of various noise and operational restraints are determined and sensitivities to some of the more important performance variables are presented for the most probable design noise and operational restraint case. Critical areas requiring new or improved technology for each cycle are delineated. (Author)
Assessment of Variable-Cycle Engines for Mach 2.7 Supersonic Transports
1976
59 pages
Report
No indication
English
Variable Cycle Engines for Advanced Supersonic Transports
SAE Technical Papers | 1975
|Variable cycle jet engines for a Mach 2.7 supersonic civil transport
Online Contents | 1998
|