ANALISIS ALIRAN TRANSONIK BERDASARKAN PERSAMAAN ATUR TRANSONIK GANGGUAN KECIL

Design of a transonic aircraft required an aerodinamics design and calculation methods to predict the aerodynamic forces in the transonic regime which is inherently nonlinear due to the pressence of the shock waves in the flow fields. This thesis describes unsteady transonic flow analysis based up...

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Bibliographic Details
Main Author: Kresna Sekar , Widjaja
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/9599
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Institution: Institut Teknologi Bandung
Language: Indonesia