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In transonic flow condition, the shock wave boundary layer interaction(SWBLI) and flow separation on wing upper surface of a civil aircraft induce transonic drag divergence. The transonic flow in case of a large drag caused by wave drag. The cause of wave drag are the strong shocks developing on the...

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Bibliographic Details
Main Author: PARLINDUNGAN HALOHO (NIM : 13605059); Tim Pembimbing: Dr. Djoko Sardjadi; Dr. Romie O. Bura; Ir., HOT
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/15955
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Institution: Institut Teknologi Bandung
Language: Indonesia

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