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Update mach tutorial wing benchmark values (#333)
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A-CGray authored Oct 8, 2024
1 parent a5276b8 commit f265bda
Showing 1 changed file with 4 additions and 4 deletions.
Original file line number Diff line number Diff line change
Expand Up @@ -14,14 +14,14 @@
# Reference values for eval functions
FUNC_REF = {
"StructAnalysis_compliance": 155444.88138037617,
"StructAnalysis_l_skin_ksFailure": 0.6688691183266002,
"StructAnalysis_l_skin_ksFailure": 0.6688752934181855,
"StructAnalysis_l_skin_mass": 1056.704174594214,
"StructAnalysis_mass": 3196.8719514874,
"StructAnalysis_rib_ksFailure": 0.25350286472639316,
"StructAnalysis_rib_ksFailure": 0.25350306610310425,
"StructAnalysis_rib_mass": 686.2303380471093,
"StructAnalysis_spar_ksFailure": 0.6336086764475523,
"StructAnalysis_spar_ksFailure": 0.6336086764052882,
"StructAnalysis_spar_mass": 400.06656937882445,
"StructAnalysis_u_skin_ksFailure": 0.46502733574612126,
"StructAnalysis_u_skin_ksFailure": 0.4650470864089127,
"StructAnalysis_u_skin_mass": 1053.8708694672512,
"AdjCon_L_SKIN_panelThicknessAdj": np.zeros(21),
"AdjCon_L_SKIN_stiffenerHeightAdj": np.zeros(21),
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