Refine
Year of publication
Institute
- Fachbereich Luft- und Raumfahrttechnik (43) (remove)
Has Fulltext
- no (43)
Document Type
- Part of a Book (43) (remove)
Keywords
- Wind Tunnel (3)
- Flight Test (2)
- Pitching Moment (2)
- Wave Drag (2)
- Aerodynamic Drag (1)
- Carsharing (1)
- Certification Rule (1)
- Drag Reduction (1)
- Electrical vehicle (1)
- Engine Efficiency (1)
- Epistemische Neugier (1)
- Evacuation Rule (1)
- Friction Drag (1)
- Ice melting probe (1)
- Ice penetration (1)
- Icy moons (1)
- Leading Edge Vortex (1)
- Mach Number (1)
- Mars (1)
- Multidisciplinary Design Optimization (1)
- Noise Exposure (1)
- Ocean worlds (1)
- Parabolized Stability Equation (1)
- Passenger compartment (1)
- Selbstwirksamkeit (1)
- Severe Accident (1)
- Sonic Boom (1)
- Specific Fuel Consumption (1)
- Supersonic Flow (1)
- Supersonic Wind Tunnel (1)
- Technology Challenge (1)
- Thermal Fatigue Testing (1)
- Thermal comfort (1)
- Thermal management (1)
- Variable Geometry (1)
- attitude dynamics (1)
- intrinsische Motivation (1)
- orbit control (1)
- orbital dynamics (1)
- sailcraft (1)
- solar sail (1)
Today the most accurate and cost effective industrial codes used in aircraft design are based on the full potential equation coupled with boundary layer equations. However, these are not capable to solve complicated three-dimensional problems of vortical flows and shocks. On the other hand Euler and Navier-Stokes codes are too expensive and not accurate enough for design purposes, especially in regard of drag and interference prediction. The reasons for these deficiencies are investigated and a way to overcome them by future developments is demonstrated.