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A method for the calculation of the lateral response of airplanes to random turbulence
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1958 |
| Description | In this method, the gust velocities are represented as rolling gusts, yawing gusts, and side gusts. Random distributions of gust velocities across the span are taken into account in defining the rolling and yawing gusts. Complex stability derivatives are used to account for the random distribution of side gusts along the fuselage and vertical tail and the lag effects in gust penetration. A sample calculation procedure is presented for obtaining the response of the airplane in each degree of freedom. |
| File Size | 15047246 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085027 |
| Archival Resource Key | ark:/13960/t9d55c86n |
| Language | English |
| Publisher Date | 1958-02-01 |
| Access Restriction | Open |
| Subject Keyword | Loads, Gust - Wings Airplanes - Components IN Combination Gusts, Turbulence Control, Lateral Stability, Lateral AND Directional - Dynamic Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
