Certification of a CFD code for high-speed civil transport design optimization
- 15 January 1996
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- A proposed methodology for computational fluid dynamics code verification, calibration, and validationPublished by Institute of Electrical and Electronics Engineers (IEEE) ,2002
- Multidisciplinary optimization of the high-speed civil transportPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Minimum-drag axisymmetric bodies in the supersonic/hypersonic flow regimesJournal of Spacecraft and Rockets, 1994
- Variable-complexity aerodynamic optimization of a high-speed civil transport wingJournal of Aircraft, 1994
- Application of a parabolized Navier-Stokes code to an HSCT configuration and comparison to wind tunnel test dataPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Aerodynamic optimization of an HSCT configuration using variable-complexity modelingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- An assessment of current methods for drag-due-to-lift minimization at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Euler analysis of a High-Speed Civil Transport concept at Mach 3Journal of Aircraft, 1991
- The pros and cons of code validationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- A supersonic maneuver wing designed for nonlinear attached flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983