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Detailed transonic flow field measurements about a supercritical airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Spaid, F. W. Roos, F. W. Stivers Jr., L. S. Hurley, F. X. Bandettini, A. |
| Copyright Year | 1975 |
| Description | The transonic flow field about a Whitcomb-type supercritical airfoil profile was measured in detail. In addition to the usual surface pressure distributions and wake surveys, schlieren photographs were taken and velocity vector profiles were determined in the upper surface boundary layer and in the near wake. Spanwise variations in the measured pressures were also determined. The data are analyzed with the aid of an inviscid transonic finite-difference computer program as well as with boundary layer modeling and calculation schemes. |
| File Size | 4050862 |
| Page Count | 66 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750018903 |
| Archival Resource Key | ark:/13960/t8jd9n97s |
| Language | English |
| Publisher Date | 1975-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Transonic Flow Airfoil Profiles Finite Difference Theory Flow Distribution Pressure Distribution Inviscid Flow Near Wakes Supercritical Wings Computer Programs Boundary Layer Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |