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The experimental determination of the moments of inertia of airplanes
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1934 |
| Description | The application of the pendulum method to the experimental determination of the moments of inertia of airplanes is discussed in this report. Particular reference is made to the effects of the air, in which the airplane is immersed, on the swinging tests and to the procedure by which these effects are taken into account. This procedure has been used for some time, and the data on several airplanes for which the moments of inertia have been found are included. |
| File Size | 1273933 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930091541 |
| Archival Resource Key | ark:/13960/t1fj5nm0f |
| Language | English |
| Publisher Date | 1934-01-01 |
| 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 |