Detail Kaji Eksperimental Dan Simulasi Visualisasi Aliran Udara Terhadap Model NACA 0012 Bibliografi Author: KURNIA, GALIH ; Ruslan, Wegie (Advisor) Topik: Visualization; Smoke; Airfoil; Separation; Gradient Velocity Bahasa: (ID )     Penerbit: Program Studi Teknik Mesin Fakultas Teknik Unika Atma Jaya     Tempat Terbit: Jakarta    Tahun Terbit: 2013     Jenis: Theses - Undergraduate Thesis Fulltext: Galih Kurnia's Undergraduate Theses.pdf (3.03MB; 8 download) Ketersediaan Perpustakaan Pusat (Semanggi) Nomor Panggil: FTM-2006 Non-tandon: tidak ada Tandon: 1  Lihat Detail Induk Abstract Not all results a manufacturing process will exactly as the design of computation. With the existence of this flow phenomena required testing at a facility testing aerodynamics capable of customize the flow of air as actual state. Testing done in experimental and simulation. Experimental methods done by analyzing position the separation and phenomena more going results testing in the open loop subsonic wind tunnel using smoke visualization on airfoils NACA 0012, while the simulation was done with the software. The test results indicate that the greater the angle of attack and its speed, then the turbulent will be bigger as a result of increase of gradient velocity of the separation that occurs Opini Anda Klik untuk menuliskan opini Anda tentang koleksi ini! Lihat Sejarah Pengadaan  Konversi Metadata   Kembali

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