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Changed Github runner from Conda to Mamba #266

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merged 30 commits into from
Nov 2, 2023
Merged

Changed Github runner from Conda to Mamba #266

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38f3f6a
Fixed typos in linear_goland_flutter.ipynb
ben-l-p Oct 25, 2023
065f71d
Merge branch 'develop' into fix_linear_goland_flutter.ipynb
ben-l-p Oct 27, 2023
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Change GitHub workflow to use macOS
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e3f7c3b
Update sharpy_no_test_needed.yaml to use macOS
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Finalise changing Github runner from conda to mamba
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10 changes: 5 additions & 5 deletions docs/source/content/example_notebooks/linear_goland_flutter.ipynb
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Original file line number Diff line number Diff line change
Expand Up @@ -23,7 +23,7 @@
"* Evaluate the stability of the linearised aeroelastic system at different velocities and plot the results.\n",
"\n",
"## Wing properties\n",
"Span: b=20 ft., chord: c=6 ft., weight: 4 psi., radius of gyration about CG: .25c, elastic axis: 0.33c,, centre of gravity: 0.43c\n",
"Span: b=20 ft., chord: c=6 ft., weight: 4 psi., radius of gyration about CG: .25c, elastic axis: 0.33c, centre of gravity: 0.43c\n",
"\n",
"### References\n",
"\n",
Expand Down Expand Up @@ -79,7 +79,7 @@
"outputs": [],
"source": [
"u_inf = 1.\n",
"alpha_deg = 2. # Define antle of attack for static aeroelastic analsis.\n",
"alpha_deg = 2. # Define angle of attack for static aeroelastic analysis.\n",
"rho = 1.02 # Air density."
]
},
Expand All @@ -100,8 +100,8 @@
"source": [
"M = 16 # Number of chordwise panels\n",
"N = 32 # Number of spanwise panels\n",
"M_star_fact = 10 # Length of the chords in chords.\n",
"num_modes = 8 # Mumber of vibration modes retained in the structural model."
"M_star_fact = 10 # Length of the wake in chords.\n",
"num_modes = 8 # Number of vibration modes retained in the structural model."
]
},
{
Expand Down Expand Up @@ -531,7 +531,7 @@
"source": [
"### Stability \n",
"\n",
"The stability of the Goland wing is now analysed under changing free stream velocity. The flutter modes involves the two lowest frequency modes near the imaginar axis (1st bending and 1st torsion if aerodynamics is removed). The two modes are seen quite separated at 100 m/s. As speed is increased, the damping of the torsion mode decreases until it crosses the imaginary axis onto the right hand plane and flutter begins."
"The stability of the Goland wing is now analysed under changing free stream velocity. The flutter modes involves the two lowest frequency modes near the imaginary axis (1st bending and 1st torsion if aerodynamics is removed). The two modes are seen quite separated at 100 m/s. As speed is increased, the damping of the torsion mode decreases until it crosses the imaginary axis onto the right hand plane and flutter begins."
]
},
{
Expand Down
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