NASA NTRS · 19940028960
HSCT noise reduction technology development at GE Aircraft Engines
Abstract
The topics covered include the following: High Speed Civil Transport (HSCT) exhaust nozzle design approaches; GE aircraft engine (GEAE) HSCT acoustics research; 2DCD non-IVP suppressor ejector; key sensitivities from reference aircraft; acoustic experiments; aero-mixing experimental set-up; fluid shield nozzle; HSCT Mach 2.4 flade nozzle; noise prediction; nozzle concept for GE/Boeing joint test; scale model hot core flow path modified to prevent hub-choking CFL3-D solution; HSCT exhaust nozzle status; and key acoustic technology issues for HSCT's.
Keep this discovery
Explore connections, maps & timelines
Majjigi, Rudramuni K.. 1992-04-01. HSCT noise reduction technology development at GE Aircraft Engines. https://ntrs.nasa.gov/citations/19940028960
Cite the original work for its findings. Save a collection to share your selection of sources.