FLIGHT LOAD ANALYSIS OF IFX FIGHTER AIRCRAFT BASED ON STATIC-AEROELASTIC APPROACH

This thesis report describes a static-aeroelastic approach for more accurately predicting the flight loading on IFX fighter aircraft structures with underwing store configurations. When this agile aircraft maneuvers, the underwing stores will cause structural deflections that changes airload dist...

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Bibliographic Details
Main Author: Eriawan, Andi
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/43483
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Institution: Institut Teknologi Bandung
Language: Indonesia
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