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Author

Pei-Jun Lai

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Conference Sep 2026

Research on flight test method for minimum control speed during approach and landing (VMCL) dynamic test in civil aircraft

This paper investigates the flight test method for the Minimum Control Speed during Approach and Landing (VMCL) dynamic test of a twin-engine narrow-body mainline airliner undergoing EASA type certification in accordance with CS- 25 requirements. The research identifies the core challenge as the significant energy stat...

Pei-Jun Lai, Hou-Shi Wang, Yuan-Tao Fu · 0 citations

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