Adapt tank definition in CSD
1 unresolved thread
1 unresolved thread
The tank definition was extended to include an additional tank and the trim tank. This shall be used to test aircraft-design!9 (merged)
Merge request reports
Activity
added aircraftCSMR-2020 moduletank_design labels
requested review from @AndiGob
assigned to @kristina.mazur
mentioned in merge request aircraft-design!9 (merged)
204 <lower_boundary>0</lower_boundary> 205 <upper_boundary>5</upper_boundary> 206 </energy_carrier_ID> 207 <location description="Component where the tank is located: fuselage, wing, horizontal_stabilizer"> 208 <value>horizontal_stabilizer</value> 209 </location> 210 <position description="Position of tank in location: tailcone, rear, front, top, bottom, center, inner_left, outer_left, inner_right, outer_right, total"> 211 <value>total</value> 212 </position> 213 <energy_share description="Share of this tanks energy in relation to required mission energy (of same energy carrier). Only relevant for liquid hydrogen tanks. Equals 0.0 for kerosene tanks."> 214 <value>0.0</value> 215 <unit>1</unit> 216 <lower_boundary>0.0</lower_boundary> 217 <upper_boundary>1.0</upper_boundary> 218 </energy_share> 219 </tank> mentioned in commit 3d958333
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