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**Describe the bug**
In lines 273, 280 and 313, according to the Aerodynamics input h5file: I think that the control surface info `['control_surface_hinge_coords']` should be `['control_surface_hin…
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Create a new design for the rocket body
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Determine the stability (Cd and Cp) calculations in regards to the geometry of the airbrake as well as in regards to the geometry of the Rocket.
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We'll see which one gets done faster: Sandia's or NREL's when Eagle is back.
Runs we will submit at Sandia:
(1) IEA 15 MW power curve (10 separate runs). Nate, Neil, Phil, Kevin.
(2) NREL 5 MW case.…
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This is probably a wontfix, but thought I'd mention that when I place a plane inside another plane for transport (ie. J3Cub inside Antonov), the J3 is affected by the wind in the same way it would be …
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Find some way to specify which stage will enter atmosphere, and don't use the parts that will be discarded during predictions. Also need to check if FAR aerodynamics is more complicated when staging t…
neuoy updated
10 months ago
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Converting the FAM and blower model from Simulink to C++, we encountered a few things that look suspicious:
- [ ] Discharge coefficients are different for the two propulsion modules
- [ ] Why the …
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```
What steps will reproduce the problem?
1. Feature not Implemented Yet
What is the expected output? What do you see instead?
A report of Aerodynamics for evaluating different body mods.
```
Origi…
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```
What steps will reproduce the problem?
1. Feature not Implemented Yet
What is the expected output? What do you see instead?
A report of Aerodynamics for evaluating different body mods.
```
Origi…
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```
What steps will reproduce the problem?
1. Feature not Implemented Yet
What is the expected output? What do you see instead?
A report of Aerodynamics for evaluating different body mods.
```
Origi…