Loading...
Please wait, while we are loading the content...
Similar Documents
Two-dimensional aerodynamic characteristics of the ames hi-120, hi-8, and low-12 airfoils
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Berchak, M. J. Gregorek, G. M. |
| Copyright Year | 1987 |
| Description | During the period between June and September 1986, the Aeronautical and Astronautical Engineering Research Laboratory (AARL) at the Ohio State University (OSU) in Columbus, Ohio, conducted tests in the 6"X22" Transonic Blowdown Wind Tunnel to determine the two-dimensional lift, drag, and pitching moment coefficients for three airfoils designated AMES HI-120, AMES LOW-12, and AMES HI-8. These tests covered a Mach number range of 0.20 to 0.86, Reynolds numbers between 2 x 10 to the 6th and 6 x 10 to the 6th powers, and angles of attack between 0 and 13 degs as directed by the NASA Project Engineer; each model was not run at every condition. This work was performed under NASA Grant NAG-2-401, Analysis of Two Advanced Transonic Airfoils. |
| File Size | 3362912 |
| Page Count | 51 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19870014156 |
| Archival Resource Key | ark:/13960/t1qg3m17t |
| Language | English |
| Publisher Date | 1987-06-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Drag Pitching Moments Transonic Flow Reynolds Number Blowdown Wind Tunnels Airfoils Two Dimensional Flow Lift Universities Wind Tunnel Tests Ohio Angle of Attack Aerodynamic Characteristics Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
