The viewgraphs for a status report of the NASA Langley Reseach Center High Speed Civil Transport (HSCT) High-Lift Research Program are provided. A listing of available models and previous wind tunnel studies are presented. Objectives and approach of the piloted simulation program are given. The HSCT High-Lift Research plans are listed and briefly described.
Status of LARC HSCT High-Lift Research
1992
29 pages
Report
No indication
English
Aircraft , Aerodynamics , Test Facilities & Equipment , Noise Pollution & Control , Aerodynamic characteristics , Aircraft configurations , Flight simulation , Lift , Noise prediction (Aircraft) , Noise reduction , Wind tunnel models , Rapid transit systems , Aircraft noise , Leading edges , Supersonic aircraft , Supersonic flight , Swept wings , Wind tunnel tests
Status of LaRC HSCT high-lift research
NTRS | 1992
|HSCT high-lift technology requirements
NTRS | 1992
|HSCT High Lift System Aerodynamic Requirements
NTIS | 1992
|HSCT high-lift aerodynamic technology requirements
AIAA | 1992
|HSCT high lift system aerodynamic requirements
NTRS | 1992
|