The High-Speed Research Program and NASA Langley Research Center sponsored the NASA High-Speed Research Program Aerodynamic Performance Workshop on February 25-28, 1997. The workshop was designed to bring together NASA and industry High-Speed Civil Transport (HSCT) Aerodynamic Performance technology development participants in area of Configuration Aerodynamics (transonic and supersonic cruise drag prediction and minimization), High-Lift, Flight Controls, Supersonic Laminar Flow Control, and Sonic Boom Prediction. The workshop objectives were to (1) report the progress and status of HSCT aerodyamic performance technology development; (2) disseminate this technology within the appropriate technical communities; and (3) promote synergy among the scientist and engineers working HSCT aerodynamics. In particular, single- and multi-point optimized HSCT configurations, HSCT high-lift system performance predictions, and HSCT Motion Simulator results were presented along with executive summaries for all the Aerodynamic Performance technology areas.
1997 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 2
1999
944 pages
Report
No indication
English
Aerodynamics , Aircraft , Fluid Mechanics , Supersonic transports , Aircraft design , Computational fluid dynamics , Aerodynamic configurations , Optimization , Aerodynamic characteristics , Performance prediction , Laminar boundary layer , Boundary layer control , Wind tunnel tests , Applications programs(Computers) , Aerodynamic drag , Drag reduction , Engine airframe integration