Vol. 2 No. 2 (2016): DESAIN KONSEPTUAL AWAL TEROWONGAN ANGIN SUPERSONIK UNTUK PROSES VALIDASI HASIL CFD DALAM PERANCANGAN PESAWAT TEMPUR KFX

In order to improve science and technology in aerospace, we need innovation for developing supersonic wind tunnel. This wind tunnel will be expected to support the development of KFX fighter aircraft, including task to analyze air flow that occurs in the aircraft. Considering the speed of current wind tunnel that only reach 2 Mach, in the future we need to develop wind tunnel whose speed can reach 3–4 Mach. This study uses CFD software as comparative data.