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Investigation of drag and static longitudinal and lateral stability characteristics of a model of a 40.4 deg swept-wing airplane at mach numbers of 1.56 and 2.06
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carmel, M. M. Turner, K. L. |
| Organization | The National Aeronautics and Space Administration (NASA) |
| Copyright Year | 1957 |
| Abstract | Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity at supersonic speeds |
| File Size | 18321231 |
| File Format | |
| Alternate Webpage(s) | http://www.archive.org/details/nasa_techdoc_19660010451 |
| Archival Resource Key | ark:/13960/t03x8zh68 |
| Language | English |
| Publisher Date | 1957-01-18 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Drag Wind Tunnel Stability Tests Wind Tunnel Tests Drag Fighter Aircraft Lateral Stability Longitudinal Stability Supersonic Speed Swept Wing Wind Tunnel Stability Test Mach Number Static Stability Swept Wings Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |