Kurikulum 2024

Kode Mata KuliahAE3102 / 4 SKS
Penyelenggara136 - Teknik Dirgantara / FTMD
KategoriKuliah
Bahasa IndonesiaEnglish
Nama Mata KuliahAerodinamikaAerodynamics
Bahan Kajian
  1. Teori Aerodinamika Linear
  2. Metode Aliran Potensial
  3. Teori Airfoil dan Sayap
  4. Prandtl Lifting line
  5. Aliran linearized (subsonik dan supersonik)
  6. Gelombang kejut dan ekspansi
  7. Aerodinamika nozzle
  8. Metode karakteristik
  9. Aerodinamika Aliran Viskos
  10. Aliran Transonik dan Hipersonik
  1. Linear Aerodynamic Theory
  2. Potential Flow Method
  3. Airfoil and Wing Theory
  4. Prandtl Lifting line
  5. Linearized flow (subsonic and supersonic)
  6. Shock and expansion wave
  7. Nozzle Aerodynamics
  8. Method of characteristics
  9. Aerodynamics of viscous flows
  10. Transonic and hypersonic flows
Capaian Pembelajaran Mata Kuliah (CPMK)
  1. Memahami pemodelan aliran potensial di sekitar benda, serta batasan penggunaan pemodelan tersebut.
  2. Menyelesaikan permasalahan aliran potensial di sekitar airfoil dan sayap, serta memahami aspek-aspek yang mempengaruhi gaya-gaya yang dihasilkan dan pengaruhnya pada konfigurasi sayap pesawat.
  3. Memahami aliran linearized untuk aerodinamika subsonik dan supersonik.
  4. Memahami dan mampu menjelaskan aerodinamika nozzle dan metode desain aerodinamika nozzle.
  5. Menggunakan metode karakteristik dalam desain dan analisis aerodinamika.
  6. Memahami fenomena aerodinamika viskos untuk perhitungan gaya-gaya aerodinamika.
  7. Menjelaskan berbagai fenomena yang terjadi pada aliran transonik dan hipersonik serta bagaimana mengatasi permasalahan yang muncul pada kedua aliran tersebut.
  1. Understand the modeling of potential flows around objects, as well as the limitations of using such modeling.
  2. Solve potential flow problems around airfoils and wings, and understand the aspects that affect the forces generated and their effect on aircraft wing configurations.
  3. Understand linearized flows for subsonic and supersonic aerodynamics.
  4. Understand and be able to explain nozzle aerodynamics and nozzle aerodynamics design methods.
  5. Using characteristic methods in aerodynamic design and analysis.
  6. Understand the phenomenon of viscous aerodynamics for the calculation of aerodynamic forces.
  7. Explain the various phenomena that occur in transonic and hypersonic flows and how to overcome the problems that arise in both flows.
Metode PembelajaranTatap muka di kelas, Tutorial materi kuliahIn-person class, lecture tutorial
Modalitas PembelajaranLuring, Sinkron, MandiriOffline, synchronous, independent
Jenis NilaiABCDE
Metode PenilaianUjian Tengah Semester, Ujian Akhir Semester, TugasMidterm Exam, Final Exam, Assignment
Catatan Tambahan