Loading...
Please wait, while we are loading the content...
Similar Documents
Pressure distribution and damping in steady roll at supersonic mach numbers of flat swept-back wing with subsonic edges
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 2008989 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082702 |
| Archival Resource Key | ark:/13960/t3sv1xf55 |
| Language | English |
| Publisher Date | 1950-03-01 |
| Access Restriction | Open |
| Subject Keyword | Rolling Moments - Wings, Sweptback Damping IN Roll Theories - Flow - Supersonic Pressure Distribution - Wings, Sweptback Theories - Wings 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 |