Mata Kuliah AE5014 - 2026

Kode Mata KuliahAE5014 / 3 SKS
Penyelenggara236 - Teknik Dirgantara / FTMD
KategoriKuliah
Bahasa IndonesiaEnglish
Nama Mata KuliahAliran KompresibelCompressible Flows
Bahan Kajian
  1. Review Aerodinamika
  2. Pengenalan ke aliran hipersonik
  3. Detonation dan Deflagration
  4. Aliran hipersonik inviscid : bidang miring dan metode berbasis medan aliran
  5. Aliran hipersonik viskos
  6. Dinamika gas temperatur tinggi
  7. Aliran inviscid temperatur tinggi equilibrium dan nonequilibrium
  8. Aliran viskos temperatur tinggi
  1. Review of Aerodynamics
  2. Introduction to Hypersonic Flows
  3. Detonation and Deflagration Phenomena
  4. Inviscid Hypersonic Flows: Oblique Surfaces and Flow-Field-Based Methods
  5. Viscous Hypersonic Flows
  6. High-Temperature Gas Dynamics
  7. Equilibrium and Nonequilibrium High-Temperature Inviscid Flows
  8. High-Temperature Viscous Flows
Capaian Pembelajaran Mata Kuliah (CPMK)
  1. Mempelajari dasar-dasar dinamika aliran hipersonik, mencakup detonasi dan deflagration, dan juga asumsi kecepatan tak hingga
  2. Melakukan analisis dan menitepretasikan hasil analitik dan hasil numerik aliran over expanded dan under expanded dibelakang exhaust nozzle
  3. Melakukan kerjasama tim dan mempresentasikan tugas kelompok dalam menganalis aliran over expanded dan under expanded dibelakang exhaust nozzle
  4. Mempelajari fenomena aliran transonik dan aliran hipersonik beserta metode pendekatan
  5. Mempelajari konsep aliran hipersonik viskos, mencakup kasus lapisan batas dan titik stagnasi
  6. Memahami konsep dinamika aliran temperatur tinggi, mencakup aliran hipersonik inviscid equilibrium dan nonequilibrium, serta aliran hipersonik viskos
  1. Understand the fundamental principles of hypersonic flow dynamics, including detonation and deflagration phenomena, as well as the infinite-velocity approximation.
  2. Analyze and interpret analytical and numerical results of over-expanded and under-expanded flows downstream of exhaust nozzles.
  3. Demonstrate effective teamwork and present group project findings related to the analysis of over-expanded and under-expanded flows downstream of exhaust nozzles.
  4. Understand transonic and hypersonic flow phenomena and the analytical and computational methods used to study them.
  5. Understand the principles of viscous hypersonic flows, including boundary-layer and stagnation-point flow phenomena.
  6. Understand the principles of high-temperature gas dynamics, including equilibrium and nonequilibrium inviscid hypersonic flows, as well as viscous hypersonic flows.
Metode PembelajaranTatap muka di kelasFace-to-face classroom instruction
Modalitas PembelajaranLuring, sinkron, mandiriIn-person synchronous learning Independent study
Jenis NilaiABCDE
Metode PenilaianUjian tengah semester Ujian akhir semester TugasMidterm Examination Final Examination Assignment
Catatan Tambahan