Loading...
Please wait, while we are loading the content...
Similar Documents
Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips : subsonic leading edges
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 1070959 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082822 |
| Archival Resource Key | ark:/13960/t6g20b40d |
| Language | English |
| Publisher Date | 1950-06-01 |
| Access Restriction | Open |
| Subject Keyword | Wings, Sweptback - Tapered Yawing Moments - Wings, Sweptback Theories - Flow - Supersonic 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 |