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Characteristics of an airfoil as affected by fabric sag
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1932 |
| Description | This report presents the results of tests made at a high value of the Reynolds Number in the N.A.C.A. variable-density wind tunnel to determine the aerodynamic characteristics of an airfoil as affected by fabric sag. Tests were made of two Gottingen 387 airfoils, one having the usual smooth surface and the other having a surface modified to simulate two types of fabric sag. The results of these tests indicate that the usual sagging of the wind covering between ribs has a very small effect on the aerodynamic characteristics of an airfoil. |
| File Size | 5826432 |
| Page Count | 10 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930081179 |
| Archival Resource Key | ark:/13960/t05x5hg6x |
| Language | English |
| Publisher Date | 1932-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Gotettingen 387 - Char , C P & Ordinates Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
