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Theory of an airplane encountering gusts iii
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1918 |
| Description | Report presents a new method for solving linear equations developed by Bromwich, which is suited to determine the motion for any particular gust, when the machine started from equilibrium, without the trouble of determining the constants of integration in the complementary function. (author) |
| File Size | 427841 |
| Page Count | 7 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930091055 |
| Archival Resource Key | ark:/13960/t57d62c5x |
| Language | English |
| Publisher Date | 1918-01-01 |
| Access Restriction | Open |
| Subject Keyword | 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 |