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Effect of thickness on the lateral force and yawing moment of a sideslipping delta wing at supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 685535 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082473 |
| Archival Resource Key | ark:/13960/t4cp1fm01 |
| Language | English |
| Publisher Date | 1949-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Thickness Theories - Flow Supersonic Sideslipping Wings, Delta - Stability Yawing Moments - Wings, Delta Theories - Flow Linear Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |