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Tables for correcting airfoil data obtained in the langley 0.3-meter transonic cryogenic tunnel for sidewall boundary-layer effects
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Adcock, J. B. Jenkins, R. V. |
| Copyright Year | 1986 |
| Description | Tables for correcting airfoil data taken in the Langley 0.3-meter Transonic Cryogenic Tunnel for the presence of sidewall boundary layer are presented. The corrected Mach number and the correction factor are minutely altered by a 20 percent change in the boundary layer virtual origin distance. The sidewall boundary layer displacement thicknesses measured for perforated sidewall inserts and without boundary layer removal agree with the values calculated for solid sidewalls. |
| File Size | 688719 |
| Page Count | 21 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860016817 |
| Archival Resource Key | ark:/13960/t04z05r0m |
| Language | English |
| Publisher Date | 1986-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Tables Data Transonic Wind Tunnels Wall Flow Wind Tunnel Tests Inserts Wind Tunnel Walls Correction Aerodynamic Characteristics Boundary Layers Cryogenic Wind Tunnels Mach Number Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |