Mata Kuliah AE4021 - 2024

Kode Mata KuliahAE4021 / 3 SKS
Penyelenggara136 - Teknik Dirgantara / FTMD
KategoriKuliah
Bahasa IndonesiaEnglish
Nama Mata KuliahBeban Pesawat UdaraAircraft Loads
Bahan Kajian
  1. Pendahuluan Beban Pesawat Udara
  2. Steady Horizontal Flight
  3. Beban Manuver
  4. Beban Turbulensi Udara (Gust)
  5. Beban di Darat
  6. Beban lain-lain
  7. Pengaruh Elastisitas
  8. Horizontal Tail Load
  9. Wing Load
  10. Structural Design Consideration
  11. Airspeeds for Structural Engineers
  1. Introduction to Aircraft Loads
  2. Steady Horizontal Flight
  3. Maneuver Loads
  4. Gust Loads
  5. Miscellaneous Loads
  6. Other expenses
  7. Elasticity Effects
  8. Horizontal Tail Load
  9. Wing Load
  10. Structural Design Consideration
  11. Airspeeds for Structural Engineers
Capaian Pembelajaran Mata Kuliah (CPMK)
  1. Mahasiswa dapat menjelaskan parameter utama (aerodinamika, prestasi terbang, dan struktur) yang mempengaruhi besar beban pesawat.
  2. Mahasiswa dapat menggambar n-V diagrams untuk manuver dan gust
  3. Mahasiswa dapat menurunkan persamaan kesetimbangan pesawat untuk kondisi terbang jelajah dan manuver
  4. Mahasiswa dapat menghitung besar beban pada sayap dan ekor akibat terbang manuver.
  5. Mahasiswa dapat menghitung beban pada saat di darat dan beban-beban lain.
  6. Mahasiswa dapat menjelaskan interaksi antara elastisitas dan aerodinamika
  7. Mahasiswa dapat menggambar distribusi gaya dalam pada komponen utama, wing, tail, dan fuselage.
  1. Students are able to explain the primary parameters (aerodynamics, flight performance, and structure) that influence aircraft load magnitude.
  2. Students are able to plot V-n diagrams for maneuver and gust conditions.
  3. Students are able to derive aircraft equilibrium equations for cruise and maneuver flight conditions.
  4. Students are able to calculate wing and tail loads resulting from flight maneuvers.
  5. Students are able to calculate ground loads and miscellaneous loads.
  6. Students are able to explain the interaction between elasticity and aerodynamics (aeroelasticity).
  7. Students are able to plot internal force distributions for major components: wing, tail, and fuselage.
Metode PembelajaranTatap mukaFace-to-face
Modalitas PembelajaranLuring Sinkron IndividuOffline, Synchronous, Independent
Jenis NilaiABCDE
Metode PenilaianTugas Ujian tengah semester Ujian akhir semesterAssignment, Midterm Exam, and Final Exam
Catatan Tambahan