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Drag reduction through higher wing loading
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kohlman, D. L. |
| Copyright Year | 1975 |
| Description | A reduction in wing area, thickness, and span increases wing loading and lowers parasitic drag for a typical light airplane by 10.5%. |
| File Size | 473102 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760003921 |
| Archival Resource Key | ark:/13960/t3hx6432t |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Aerodynamic Drag Airfoil Profiles Drag Reduction General Aviation Aircraft Wing Loading Light Aircraft Aircraft Configurations Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |