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Flight-determined lag of angle-of-attack and angle-of-sideslip sensors in the yf-12a airplane from analysis of dynamic maneuvers
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Gilyard, G. B. Belte, D. |
| Copyright Year | 1974 |
| Description | Magnitudes of lags in the pneumatic angle-of-attack and angle-of-sideslip sensor systems of the YF-12A airplane were determined for a variety of flight conditions by analyzing stability and control data. The three analysis techniques used are described. An apparent trend with Mach number for measurements from both of the differential-pressure sensors showed that the lag ranged from approximately 0.15 second at subsonic speed to 0.4 second at Mach 3. Because Mach number was closely related to altitude for the available flight data, the individual effects of Mach number and altitude on the lag could not be separated clearly. However, the results indicated the influence of factors other than simple pneumatic lag. |
| File Size | 1104759 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740026347 |
| Archival Resource Key | ark:/13960/t18m2308m |
| Language | English |
| Publisher Date | 1974-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Flight Tests Error Analysis Data Acquisition Aircraft Performance Data Processing Instrument Errors Flight Instruments Angle of Attack Fighter Aircraft Sideslip Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
