AERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER

The advancements in aerospace engineering has made aircrafts capable of traveling at high speed. As flow regions beyond the speed of sound, a different design method is employed for designing high speed aircrafts. Additionally, conventional aircrafts tend to perform worse in supersonic or hyperso...

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Main Author: Fathin Humairah, Jessica
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/71502
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:71502
spelling id-itb.:715022023-02-10T14:48:25ZAERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER Fathin Humairah, Jessica Indonesia Final Project power-law waverider, oblique shock theory, hypersonic flow INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/71502 The advancements in aerospace engineering has made aircrafts capable of traveling at high speed. As flow regions beyond the speed of sound, a different design method is employed for designing high speed aircrafts. Additionally, conventional aircrafts tend to perform worse in supersonic or hypersonic regimes. Therefore, the waverider was introduced to solve those problems. The powerlaw waverider shape was created using a MATLAB code. Ansys CFX is then used to simulate the waverider’s aerodynamic performance, in which the results were then analyzed quantitatively and qualitatively. The numerical solutions obtained were also compared to the analytical results. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description The advancements in aerospace engineering has made aircrafts capable of traveling at high speed. As flow regions beyond the speed of sound, a different design method is employed for designing high speed aircrafts. Additionally, conventional aircrafts tend to perform worse in supersonic or hypersonic regimes. Therefore, the waverider was introduced to solve those problems. The powerlaw waverider shape was created using a MATLAB code. Ansys CFX is then used to simulate the waverider’s aerodynamic performance, in which the results were then analyzed quantitatively and qualitatively. The numerical solutions obtained were also compared to the analytical results.
format Final Project
author Fathin Humairah, Jessica
spellingShingle Fathin Humairah, Jessica
AERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER
author_facet Fathin Humairah, Jessica
author_sort Fathin Humairah, Jessica
title AERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER
title_short AERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER
title_full AERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER
title_fullStr AERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER
title_full_unstemmed AERODYNAMIC DESIGN AND ANALYSIS OF POWER-LAW DERIVED HYPERSONIC WAVERIDER
title_sort aerodynamic design and analysis of power-law derived hypersonic waverider
url https://digilib.itb.ac.id/gdl/view/71502
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