Changed numbers in stress calcs (also testing commit signing)
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1 changed files with 21 additions and 4 deletions
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@ -115,16 +115,33 @@ print(f"Bending Moment at of 1 Wing from root: {bending_moment_wing:.4f} Nm\n")
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# Max Stress Calcs
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B = 4 * 0.001 # Width in m
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D = 4 * 0.001 # Height or depth in m
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# 4mm Spars
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area_moment_inertia = ((0.004) * (0.004**3))/12
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area_moment_inertia = ((B) * (D**3))/12
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print(f"Second moment of inertia for 4mm: {area_moment_inertia} m^4")
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max_stress = bending_moment_wing * ((2*(10**-3)) / area_moment_inertia)
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max_stress = bending_moment_wing * ((D/2) / area_moment_inertia)
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print(f"Max Stress for 4mm spar: {max_stress:.4f} Pa or {max_stress/1000000:.4f} MPa")
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B = 6 * 0.001 # Width in m
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D = 6 * 0.001 # Height or depth in m
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# 6mm Spars
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area_moment_inertia = ((0.006) * (0.006**3))/12
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area_moment_inertia = ((B) * (D**3))/12
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print(f"Second moment of inertia for 6mm: {area_moment_inertia} m^4")
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max_stress = bending_moment_wing * ((3*(10**-3)) / area_moment_inertia)
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max_stress = bending_moment_wing * ((D/2) / area_moment_inertia)
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print(f"Max Stress for 6mm spar: {max_stress:.4f} Pa or {max_stress/1000000:.4f} MPa")
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B = 12 * 0.001 # Width in m
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D = 2 * 0.001 # Height or depth in m
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# 6mm Spars
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area_moment_inertia = ((B) * (D**3))/12
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print(f"Second moment of inertia for new test: {area_moment_inertia} m^4")
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max_stress = bending_moment_wing * ((D/2) / area_moment_inertia)
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print(f"Max Stress for new test spar: {max_stress:.4f} Pa or {max_stress/1000000:.4f} MPa")
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