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A numerical simulation of three-dimensional flow in an adaptive wall wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mendoza, J. P. |
| Copyright Year | 1984 |
| Description | Numerical simulations of three dimensional flows in a prototype adaptive wall wind tunnel are conducted at the Mach number of 0.6 to investigate: (1) wind tunnel wall interference, (2) active streamline control by varying air removal or injection along the walls, and (3) to develop a method for establishing wall boundary conditions for interference free flows. Wind tunnel wall interference could be controlled by using only the vertical velocity components. For the configuration tested, interference free flow with solid sidewalls can be approximated by using only floor and ceiling blowing/suction. |
| File Size | 1012677 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840020681 |
| Archival Resource Key | ark:/13960/t9g49j73m |
| Language | English |
| Publisher Date | 1984-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Wind Tunnels Three Dimensional Flow Prototypes Wind Tunnel Tests Aerodynamic Interference Analysis Mathematics Wind Tunnel Models Computerized Simulation Wind Tunnel Walls Velocity Measurement Active Control Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
