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Missile is the vehicle which capable of being thrown or projected to strike distant object. Specifically for supersonic missile will occur shock wave and expansion wave at around missile. This will contribute the other drag known as wave drag. Increment of drag will need more of fuel to achieve a sa...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/16802 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |
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id-itb.:168022017-10-09T10:33:27Z#TITLE_ALTERNATIVE# SITORUS (NIM : 13605026); Pembimbing: Dr. Djoko Sardjadi; Pembimbing 2 : Dr. Romie O Bura, PARLIN Indonesia Final Project INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/16802 Missile is the vehicle which capable of being thrown or projected to strike distant object. Specifically for supersonic missile will occur shock wave and expansion wave at around missile. This will contribute the other drag known as wave drag. Increment of drag will need more of fuel to achieve a same range. But the space of fuel at missile is limited. So the one way to reduce the space of fuel is reduce the fuel which needed of missile by reduce the drag. Reduction of drag is done with adding the spike at missile. Using the spike is hoped can reduce wave drag, so the total drag can be reduced. Finally the fuel which used will be reduce for the same <br /> <br /> <br /> <br /> <br /> range. 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 |
Missile is the vehicle which capable of being thrown or projected to strike distant object. Specifically for supersonic missile will occur shock wave and expansion wave at around missile. This will contribute the other drag known as wave drag. Increment of drag will need more of fuel to achieve a same range. But the space of fuel at missile is limited. So the one way to reduce the space of fuel is reduce the fuel which needed of missile by reduce the drag. Reduction of drag is done with adding the spike at missile. Using the spike is hoped can reduce wave drag, so the total drag can be reduced. Finally the fuel which used will be reduce for the same <br />
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range. |
| format |
Final Project |
| author |
SITORUS (NIM : 13605026); Pembimbing: Dr. Djoko Sardjadi; Pembimbing 2 : Dr. Romie O Bura, PARLIN |
| spellingShingle |
SITORUS (NIM : 13605026); Pembimbing: Dr. Djoko Sardjadi; Pembimbing 2 : Dr. Romie O Bura, PARLIN #TITLE_ALTERNATIVE# |
| author_facet |
SITORUS (NIM : 13605026); Pembimbing: Dr. Djoko Sardjadi; Pembimbing 2 : Dr. Romie O Bura, PARLIN |
| author_sort |
SITORUS (NIM : 13605026); Pembimbing: Dr. Djoko Sardjadi; Pembimbing 2 : Dr. Romie O Bura, PARLIN |
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| url |
https://digilib.itb.ac.id/gdl/view/16802 |
| _version_ |
1820745460623605760 |