Uji Layar RC-Model Kapal Bersayap Konfigurasi Sayap dan Step Berbeda  

Oleh:

Syamsuar, Sayuti

Jenis: Article from Journal - ilmiah nasional - tidak terakreditasi DIKTI
Dalam koleksi: JSTI: Jurnal Sains dan Teknologi Indonesia vol. 8 no. 2 (Aug. 2006), page 97-104.
Topik: RC Model; Surface Effect; Dynamic Cushion; Wing Chord; Hull; Step; Global Positioning System; Control Surface

Ketersediaan

Perpustakaan Pusat (Semanggi) Nomor Panggil: SS57.1 Non-tandon: 1 (dapat dipinjam: 0) Tandon: tidak ada

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Isi artikel

The remote control (RC) model testing of several configurations of Wing In Surface Effect craft had been beginning from design analysis, technical drawing, aerodynamics wind tunnel, hydrodynamic and RC model test. The mathematical model of Wing In Surface craft is introduced to solve the dynamics problem during takeoff, cruise and landing maneuvres. The theoretical background of hydrodynamic on hull during ground roll calculated by Savitsky method. And the aerodynamic parameters are calculated by Vortex Lattice Method (VLM) and DATCOM software. The WiSE-craft model flown from lower altitude on the sea level within the speed, V at lower altitude. The wing configurations and step positions of RC models are tested in Jatiluhur to known the dynamic characteristics. One of them is the zig zag manuvre data that recorded by GPS.

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