1998 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 2
1998 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 2
NASA's High-Speed Research Program sponsored the 1998 Aerodynamic Performance Technical Review on February 9-13, in Los Angeles, California. The review was designed to bring together NASA and industry High-Speed Civil Transport (HSCT) Aerodynamic Performance technology development participants in areas of Configuration Aerodynamics (transonic and supersonic cruise drag prediction and minimization), High-Lift, and Flight Controls. The review objectives were to (1) report the progress and status of HSCT aerodynamic performance technology development; (2) disseminate this technology within the appropriate technical communities; and (3) promote synergy among the scientists and engineers working HSCT aerodynamics. In particular, single and multi-point optimized HSCT configurations, HSCT high-lift system performance predictions, and HSCT simulation results were presented along with executive summaries for all the Aerodynamic Performance technology areas. The HSR Aerodynamic Performance Technical Review was held simultaneously with the annual review of the following airframe technology areas: Materials and Structures, Environmental Impact, Flight Deck, and Technology Integration. Thus, a fourth objective of the Review was to promote synergy between the Aerodynamic Performance technology area and the other technology areas of the HSR Program.
Document information
1998 NASA High-Speed Research Program Aerodynamic Performance Workshop, Volume 1 Part 2
1999
954 pages
Report
No indication
English
Aerodynamics , High speed , Civil aviation , Aerodynamic configurations , Optimization , Engine airframe integration , Aircraft design , Supersonic transports , Computational fluid dynamics , Canard configurations , Design analysis , Nacelles , Diverters , Aeroelasticity , Aircraft control , Aircraft stability , Navier-stokes equation , Computerized simulation