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Pressure distribution and damping in steady pitch at supersonic mach numbers of flat swept-back wings having all edges subsonic
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 2210206 |
| Page Count | 63 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082846 |
| Archival Resource Key | ark:/13960/t2j71sd5d |
| Language | English |
| Publisher Date | 1950-10-01 |
| Access Restriction | Open |
| Subject Keyword | Wings, Flat Supersonic Wings, Sweptback - Stability, Longitudinal Conical Linear Wing Tips Theories - Flow Damping IN Pitch Pressure Distribution - Wings, Sweptback Theories - Wings 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 |