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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| 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 |
| Summary: | 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.
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