Activity for Josh Hyattâ€
Type | On... | Excerpt | Status | Date |
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Comment | Post #284862 |
@#8049a Origin of thrust for the $n$'th engine is denoted $r_n$ in my scenario. It's also not quite as simple as it looks at first. Consider identical engines pointed the same direction. Easy to see the effective center of thrust is right between the two. Now throttle one of those engines down to 50%... (more) |
— | over 2 years ago |