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Analytical study of the performance of a gust alleviation system for a stol airplane
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Oehman, W. I. |
| Copyright Year | 1973 |
| Description | An analytical study has shown that a gust alleviation system for a STOL airplane in a cruise condition could reduce the root mean square of the normal acceleration of the airplane flying in random turbulence by as much as 50 percent. This alleviation is obtained by driving the flaps in response to normal acceleration and by moving the elevator in proportion to the commanded flap deflection angle and to a pitch-rate signal. |
| File Size | 962094 |
| Page Count | 42 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730011286 |
| Archival Resource Key | ark:/13960/t9f52f86n |
| Language | English |
| Publisher Date | 1973-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Aerodynamic Configurations Atmospheric Turbulence Gust Alleviators Aircraft Performance Short Takeoff Aircraft Gust Loads Aerodynamic Characteristics Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
