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Normal Force Curve Slope at 0° Angle of Attack

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February 6, 2024, 04:36	Normal Force Curve Slope at 0° Angle of Attack	#1
Air Owe New Member Join Date: Jan 2024 Posts: 1 Rep Power: 0	Hi everyone. I'm trying to validate my CFD model using results from A. Dunn, Aeropredictive methods for missile analysis, 1989. One of the results is the "Normal force curve slope". How would I obtain this as an output from Fluent? My understanding is that there is no normal force generated on a symmetric 'spinner' body at 0° AoA, so I am a bit confused and haven't found any good explanations online. Thanks

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