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Nasa supercritical airfoils: a matrix of family-related airfoils
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Harris, Charles D. |
| Copyright Year | 1990 |
| Description | The NASA supercritical airfoil development program is summarized in a chronological fashion. Some of the airfoil design guidelines are discussed, and coordinates of a matrix of family related supercritical airfoils ranging from thicknesses of 2 to 18 percent and over a design lift coefficient range from 0 to 1.0 are presented. |
| File Size | 3292872 |
| Page Count | 76 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19900007394 |
| Archival Resource Key | ark:/13960/t5q866w6r |
| Language | English |
| Publisher Date | 1990-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Thickness Supercritical Airfoils Transonic Speed Aerodynamic Coefficients Aircraft Design Aerodynamic Characteristics Lift Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |