The minimum control speed on air, VMCA (static and dynamic) of real aircraft due to wing in surface effect craft performance test

Sayuti, Syamsuar (2004) The minimum control speed on air, VMCA (static and dynamic) of real aircraft due to wing in surface effect craft performance test. Technical Report. Badan Pengkajian dan Penerapan Teknologi, Jakarta. (Unpublished)

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Item Type:	Monograph (Technical Report)
Subjects:	Aeronautics & Aerodynamics > Aircraft
Divisions:	OR_Energi_dan_Manufaktur > Teknologi_Transportasi
Depositing User:	Rasty -
Date Deposited:	10 Jun 2026 03:05
Last Modified:	10 Jun 2026 03:05
URI:	https://karya.brin.go.id/id/eprint/38762

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