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Two-measured variable method for wall interference assessment/correction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lo, C. F. Sickles, W. L. |
| Copyright Year | 1989 |
| Description | An iterative method for wall interference assessment and/or correction is presented for transonic flow conditions in wind tunnels equipped with two component velocity measurements on a single interface. The iterative method does not require modeling of the test article and tunnel wall boundary conditions. Analytical proof for the convergence and stability of the iterative method is shown in the subsonic flow regime. The numerical solutions are given for both 2-D and axisymmetrical cases at transonic speeds with the application of global Mach number correction. |
| File Size | 455210 |
| Page Count | 14 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890011588 |
| Archival Resource Key | ark:/13960/t2b905c7x |
| Language | English |
| Publisher Date | 1989-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Transonic Flow Iterative Solution Computational Fluid Dynamics Flow Distribution Aerodynamic Interference Transonic Speed Boundary Conditions Aircraft Design Wind Tunnel Walls Velocity Measurement Numerical Stability Boundary Layer Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
