Loading...
Please wait, while we are loading the content...
Similar Documents
Pressure distribution data from tests of 2.29-meter (7.5-ft.) span eet high-lift research model in langley 4- by 7-meter tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Morgan Jr., H. L. |
| Copyright Year | 1982 |
| Description | A 2.29 m (7.5 ft.) span high-lift research model equipped with full-span leading-edge slat and part-span double-slotted trailing-edge flap was tested in the Langley 4- by 7-Meter Tunnel to determine the low speed performance characteristics of a representative high aspect ratio suprcritical wing. These tests were performed in support of the Energy Efficient Transport (EET) program which is one element of the Aircraft Energy Efficiency (ACEE) project. Static longitudinal forces and moments and chordwise pressure distributions at three spanwise stations were measured for cruise, climb, two take-off flap, and two landing flap wing configurations. The tabulated and plotted pressure distribution data is presented without analysis or discussion. |
| File Size | 16674064 |
| Page Count | 545 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840020670 |
| Archival Resource Key | ark:/13960/t3130q72r |
| Language | English |
| Publisher Date | 1982-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Tables Data High Aspect Ratio Body-wing Configurations Transport Aircraft Wind Tunnel Tests Pressure Distribution Supercritical Wings Airfoils Cruising Flight Acee Program Aerodynamic Loads Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
