Implications of Recent Rotary Rig Results for Flight Prediction
Analysis of rotary balance data on a generic aircraft model revealed the nature of the flow mechanisms present in subscale experiments, which included the existence of support interference. Recent results on the F/A-18 confirmed the existence of a threshold rotation rate in the rotary data and revea...
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| Veröffentlicht in: | Journal of aircraft 2000-07, Vol.37 (4), p.545-553 |
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| container_end_page | 553 |
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| container_issue | 4 |
| container_start_page | 545 |
| container_title | Journal of aircraft |
| container_volume | 37 |
| creator | Beyers, Martin E Ericsson, Lars E |
| description | Analysis of rotary balance data on a generic aircraft model revealed the nature of the flow mechanisms present in subscale experiments, which included the existence of support interference. Recent results on the F/A-18 confirmed the existence of a threshold rotation rate in the rotary data and revealed that in the nonlinear domain at elevated angles of attack, alternatively deterministic or chaotic behavior will prevail, depending on whether or not the magnitude of the initial rotation rate exceeds the threshold value. |
| doi_str_mv | 10.2514/2.2643 |
| format | Article |
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| fulltext | fulltext |
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| ispartof | Journal of aircraft, 2000-07, Vol.37 (4), p.545-553 |
| issn | 0021-8669 1533-3868 |
| language | eng |
| recordid | cdi_aiaa_journals_10_2514_2_2643 |
| source | Alma/SFX Local Collection |
| subjects | Aerodynamics Air transportation and traffic Applied sciences Exact sciences and technology Fluid dynamics Ground, air and sea transportation, marine construction Military aircraft Wind tunnels |
| title | Implications of Recent Rotary Rig Results for Flight Prediction |
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