摘要: The third phase of a flight evaluation of a digital electronic engine control system in an F-15 has recently been completed. It was found that digital electronic engine control software logic changes and augmentor hardware improve... 展开
作者 | Burcham, F. W. Myers, L. P. Zeller, J. R. | ||
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原报告号 | N83-22201 | 总页数 | 12 |
报告类别/文献类型 | NASA / NTIS科技报告 | ||
关键词 | Airborne/spaceborne computers Avionics Electronic control Engine control F-15 aircraft Flight tests Engine design Logic design Nozzles Numerical control |