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Subsonic stability and control derivatives for an unpowered, remotely piloted 3/8-scale f-15 airplane model obtained from flight test
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Maine, R. E. Iliff, K. W. Shafer, M. F. |
| Copyright Year | 1976 |
| Description | In response to the interest in airplane configuration characteristics at high angles of attack, an unpowered remotely piloted 3/8-scale F-15 airplane model was flight tested. The subsonic stability and control characteristics of this airplane model over an angle of attack range of -20 to 53 deg are documented. The remotely piloted technique for obtaining flight test data was found to provide adequate stability and control derivatives. The remotely piloted technique provided an opportunity to test the aircraft mathematical model in an angle of attack regime not previously examined in flight test. The variation of most of the derivative estimates with angle of attack was found to be consistent, particularly when the data were supplemented by uncertainty levels. |
| File Size | 1621703 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760008088 |
| Archival Resource Key | ark:/13960/t9q28pv3f |
| Language | English |
| Publisher Date | 1976-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Stability And Control Aircraft Models Flight Tests Subsonic Speed F-15 Aircraft Remotely Piloted Vehicles Stability Derivatives 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 |
