Fix things?
This commit is contained in:
parent
0c6d48283a
commit
31aeb58d56
58
main.py
58
main.py
@ -257,9 +257,7 @@ if __name__ == '__main__':
|
||||
pressure = this_data[0]
|
||||
|
||||
# Extrapolate Aerofoil Tip
|
||||
p1 = (PITOT_PLACEMENT[9], pressure.iloc[9])
|
||||
p2 = (PITOT_PLACEMENT[18], pressure.iloc[18])
|
||||
pN = (0.9*CHORD_LEN, p2[1] + (p1[1]-p2[1])/2)
|
||||
p1, p2, pN = this_data[-3]
|
||||
|
||||
plts = (
|
||||
{"x": PITOT_PLACEMENT[:10], "y":pressure[:10], "colour": c["color"]},
|
||||
@ -296,9 +294,7 @@ if __name__ == '__main__':
|
||||
pressure = this_data[0]
|
||||
|
||||
# Extrapolate Aerofoil Tip
|
||||
p1 = (PITOT_PLACEMENT[9], pressure.iloc[9])
|
||||
p2 = (PITOT_PLACEMENT[18], pressure.iloc[18])
|
||||
pN = (0.9*CHORD_LEN, p2[1] + (p1[1]-p2[1])/2)
|
||||
p1, p2, pN = this_data[-3]
|
||||
|
||||
plts = (
|
||||
{"x": PITOT_PLACEMENT[:10], "y":pressure[:10], "colour": c["color"]},
|
||||
@ -318,34 +314,34 @@ if __name__ == '__main__':
|
||||
makeGraph(graph, False, figSavePath="./images/pressure/__{0}.png")
|
||||
|
||||
|
||||
if True:
|
||||
aoa = [a[-2] for a in cp_pain_data][1::2]
|
||||
forces = [a[-1] for a in cp_pain_data][1::2]
|
||||
# Force Graphs
|
||||
graph = {
|
||||
"title": f"All Total, Lift & Drag Forces\nfor a Clark Y 14% Aerofoil at:\n{raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m/s)",
|
||||
"windowTitle": f"All Total, Lift and Drag Forces for a Clark Y 14 Percent Airfoil - {raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m_s",
|
||||
"xLabel": "Attack Angle [$\\alpha$]",
|
||||
"yLabel": "Force [N]",
|
||||
"grid": True,
|
||||
"ledgLoc": 1,
|
||||
"plots": [
|
||||
{"x":aoa, "y":[f[0] for f in forces], "label":"Total Force"},
|
||||
{"x":aoa, "y":[f[1] for f in forces], "label":"Lift"},
|
||||
{"x":aoa, "y":[f[2] for f in forces], "label":"Drag"},
|
||||
]
|
||||
}
|
||||
if True:
|
||||
aoa = [a[-2] for a in cp_pain_data][1::2]
|
||||
forces = [a[-1] for a in cp_pain_data][1::2]
|
||||
# Force Graphs
|
||||
graph = {
|
||||
"title": f"All Total, Lift & Drag Forces\nfor a Clark Y 14% Aerofoil at:\n{raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m/s)",
|
||||
"windowTitle": f"All Total, Lift and Drag Forces for a Clark Y 14 Percent Airfoil - {raw_data["rpm"]:d}rpm - {raw_data["airSpeed"]:.1f}m_s",
|
||||
"xLabel": "Attack Angle [$\\alpha$]",
|
||||
"yLabel": "Force [N]",
|
||||
"grid": True,
|
||||
"ledgLoc": 1,
|
||||
"plots": [
|
||||
{"x":aoa, "y":[f[0] for f in forces], "label":"Total Force"},
|
||||
{"x":aoa, "y":[f[1] for f in forces], "label":"Lift"},
|
||||
{"x":aoa, "y":[f[2] for f in forces], "label":"Drag"},
|
||||
]
|
||||
}
|
||||
|
||||
makeGraph(graph, False, figSavePath="./images/{0}.png", closeFig=True)
|
||||
makeGraph(graph, False, figSavePath="./images/{0}.png", closeFig=True)
|
||||
|
||||
|
||||
print("\n\n")
|
||||
print(raw_data["rpm"])
|
||||
print("AoA Total Lift Drag ---- Upper Force Lower Force ")
|
||||
for aoa, force in [(a[-2], a[-1]) for a in cp_pain_data]:
|
||||
print(f"{aoa:d}\\textdegree & {force[0]:.3f} & {force[1]:.3f} & {force[2]:.3f} -- {force[4]:.3f} {force[5]:.3f} \\\\")
|
||||
print("-"*50)
|
||||
print("\n\n")
|
||||
print("\n\n")
|
||||
print(raw_data["rpm"])
|
||||
print("AoA Total Lift Drag ---- Upper Force Lower Force ")
|
||||
for aoa, force in [(a[-2], a[-1]) for a in cp_pain_data]:
|
||||
print(f"{aoa:d}\\textdegree & {force[0]:.3f} & {force[1]:.3f} & {force[2]:.3f} -- {force[4]:.3f} {force[5]:.3f} \\\\")
|
||||
print("-"*50)
|
||||
print("\n\n")
|
||||
|
||||
print("Generating Cp Graphs")
|
||||
|
||||
|
Loading…
Reference in New Issue
Block a user