YF-16 air induction system design loads associated with engine surge
Basic data and procedures used to calculate structural loads due to engine surge on the YF-16 prototype fighter are presented. The procedure is based on a correlation of transient-pressure vs engine-compressor pressure ratio and relies heavily on extensive flight-measured transient-pressure data fro...
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| Veröffentlicht in: | Journal of aircraft 1975-04, Vol.12 (4), p.205-209 |
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| Hauptverfasser: | , |
| Format: | Artikel |
| Sprache: | eng |
| Online-Zugang: | Volltext |
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