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Aerodynamic data from a two-dimensional cambered airfoil section in a shallow transonic flexible walled test section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wolf, S. W. D. |
| Copyright Year | 1982 |
| Description | Further flexible wall technique validation in two dimensional testing was carried out with the transonic self streamlining wind tunnel (TSWT) using a cambered NPL 9510 section. |
| File Size | 2580486 |
| Page Count | 148 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19830005799 |
| Archival Resource Key | ark:/13960/t4hn02f2q |
| Language | English |
| Publisher Date | 1982-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Flexible Bodies Aerodynamic Configurations Cambered Wings Data Acquisition Wind Tunnel Tests Wind Tunnel Walls Two Dimensional 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 |