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Navier-stokes computations of longitudinal forces and moments for a blended wing body
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Vicroy, Dan D. Pao, S. Paul Fremaux, C. Michael Biedron, Robert T. Park, Michael A. |
| Copyright Year | 2004 |
| Description | The object of this paper is to investigate the feasibility of applying CFD methods to aerodynamic analyses for aircraft stability and control. The integrated aerodynamic parameters used in stability and control, however, are not necessarily those extensively validated in the state of the art CFD technology. Hence, an exploratory study of such applications and the comparison of the solutions to available experimental data will help to assess the validity of the current computation methods. In addition, this study will also examine issues related to wind tunnel measurements such as measurement uncertainty and support interference effects. Several sets of experimental data from the NASA Langley 14x22-Foot Subsonic Tunnel and the National Transonic Facility are presented. Two Navier-Stokes flow solvers, one using structured meshes and the other unstructured meshes, were used to compute longitudinal static stability derivatives for an advanced Blended Wing Body configuration over a wide range of angles of attack. The computations were performed for two different Reynolds numbers and the resulting forces and moments are compared with the above mentioned wind tunnel data. |
| File Size | 6482292 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20050041825 |
| Archival Resource Key | ark:/13960/t85j2gw65 |
| Language | English |
| Publisher Date | 2004-12-28 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Thermodynamics Pitching Moments Degrees of Freedom Computational Fluid Dynamics Unstructured Grids Mathematics Reynolds Number Blended-wing-body Configurations Computerized Simulation Longitudinal Stability Navier-stokes Equation Subsonic Wind Tunnels Wind Tunnel Tests Control Stability Support Interference Angle of Attack Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |