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The damping due to roll of triangular, trapezoidal, and related plan forms in supersonic flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 11623960 |
| Page Count | 26 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082350 |
| Archival Resource Key | ark:/13960/t5w70sv7r |
| Language | English |
| Publisher Date | 1948-03-01 |
| Access Restriction | Open |
| Subject Keyword | Wings, Delta Theories - Wings Damping IN Roll Load Distribution ,wing-span Downwash Theories - Flow - Supersonic Wings, Rectangular Wings, Sweptback Wings - Stability 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 |