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Now just need venting...\r\n\r\n* Removed arccos from heat into propellant to vastly increase robustness but slightly decrease accuracy\r\n\r\n* Added venting and heating features to tank, updated tests\r\n\r\n* Fixed deprecation error in ExecComp\r\n\r\n* Added validation for LH2 tank\r\n\r\n* Added ability to pull LH2 from tank in addition from GH2\r\n\r\n* Added lower bound to ullage temperature\r\n\r\n* Added lower bound to pressure in ullage ODE\r\n\r\n* Added more bounds for physical behavior\r\n\r\n* Updated defaults of LH2 tank to better reflect real world\r\n\r\n* Updated LH2 tank tests for new default options\r\n\r\n* Small change to LH2 tank docs\r\n\r\n* Removed TMS to match mdolab/master\r\n\r\n* Ran black\r\n\r\n* Added proper validation script for MHTB boil-off\r\n\r\n* Working on new boil off model\r\n\r\n* Boil off model gets reasonable results, needs testing, cleanup, and verification of ODE\r\n\r\n* Cleaned up boil off API and improved initial guess for solver\r\n\r\n* Added tests and fixed derivatives for fill level calc\r\n\r\n* Tested boil off ODE against EBM\r\n\r\n* Added derivatives for hydrogen property functions\r\n\r\n* Analytic derivatives for half of the boil of ODE outputs\r\n\r\n* Analytic derivatives for V_dot_gas in boil off ODE\r\n\r\n* Added derivatives for T_dot_liq\r\n\r\n* Analytic partials for boil off ODE done\r\n\r\n* Fixed incorrect derivative when T_dot_liq is zeroed out\r\n\r\n* Boil off with complex step to check works great now\r\n\r\n* New structural model for vacuum tank\r\n\r\n* Added air thermal conductivity\r\n\r\n* Added viscosity\r\n\r\n* Ran black\r\n\r\n* Added vacuum wall model\r\n\r\n* Starting new thermal model\r\n\r\n* Getting thermal model together, still need to make it work\r\n\r\n* Thermal model is done-ish\r\n\r\n* First pass at final tank, needs robustness and some other stuff\r\n\r\n* Added MLI weight\r\n\r\n* Added tests for LH2 tank\r\n\r\n* Trying to improve robustness of the boil-off\r\n\r\n* Added integrated test for boil off model\r\n\r\n* Removed previous versions of files for LH2 tank\r\n\r\n* Added rubberized turbofan that can do hydrogen\r\n\r\n* Added options to LH2 tank for more customizability\r\n\r\n* Consistent radius default\r\n\r\n* Trying to figure out what's going on with the solvers and guess_nonlinear\r\n\r\n* Adjusted tolerance on LH2Tank NLBGS solver\r\n\r\n* Boil off model should now work with mission integrator linking properly\r\n\r\n* LH2 tank test was failing because there was no top level nonlinear solver after NLBGS was removed\r\n\r\n* Actually....I added back in the NLBGS solver because the Newton was getting funny results\r\n\r\n* Working on improving the tank model robustness\r\n\r\n* Added some notes for myself and corrected a docstring\r\n\r\n* Added LH2 tank without boil-off model\r\n\r\n* Added tests for new LH2 tank comps\r\n\r\n* Added LH2 tanks to based energy storage imports\r\n\r\n* Removed viscosity and conductivity comps\r\n\r\n* New boil off model, still needs robustness improvement and derivatives\r\n\r\n* Fixed error in boil off\r\n\r\n* adding SOFC fuel cell model\r\n\r\n* adding sizing functions, fuel cell PEM, and updating SOFC\r\n\r\n* Adding Venkats sizing file, does not run\r\n\r\n* Making some fixes in sizing stuff\r\n\r\n* Fixed wing weight typo in init\r\n\r\n* First pass at fixed jet transport weight model\r\n\r\n* Updated docstrings and init file\r\n\r\n* Vastly improved jet transport weight estimation\r\n\r\n* Fixing up sizing example\r\n\r\n* First pass at jet transport drag buildup\r\n\r\n* Added tests for new drag buildup\r\n\r\n* Tests for geometry comps\r\n\r\n* Cylinder wetted area component\r\n\r\n* No more approximation of tail lever arm\r\n\r\n* Added tests and docstrings for tail volume coefficient sizing\r\n\r\n* Added CL max estimation\r\n\r\n* Removing old sizing\r\n\r\n* Modified RubberizedTurbofan to take in rated thrust instead of number of engines\r\n\r\n* Moved 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coefficient estimation via the critical section method\r\n\r\n* Added todo\r\n\r\n* Ran black\r\n\r\n* Removed some unused imports\r\n\r\n* Minor changes to critical section method\r\n\r\n* Added Schur solver for critical section CL max\r\n\r\n* Reduced landing gear CD for BWB\r\n\r\n* Added output documentation for BWB weights\r\n\r\n* Removed CODEOWNERS to avoid unneccesary PR reviews while developing hyfi, ADD BACK BEFORE PUSH TO MAIN\r\n\r\n* Utility to compute mean aerodynamic chord of OpenAeroStruct section-defined wing\r\n\r\n* Forgot a summation in MAC calc\r\n\r\n* Fixed docstrings\r\n\r\n* Added comps to compute wave drag\r\n\r\n* Fix a bug in the wave drag calculation\r\n\r\n* Fix error in flap CLmax calculation\r\n\r\n* Extension to critical section method (#54)\r\n\r\n* Restructure\r\n\r\n* Extended critical section method to handle varying Clmax across span\r\n\r\n* Added thermal tests back\r\n\r\n* Corrected heat leak multiplier in thermal calcs\r\n\r\n* Removed stale code and other code that is not ready to merge\r\n\r\n* Fixed BWB test\r\n\r\n* Fixed options in BWB test\r\n\r\n* One more bit of code not ready to merge\r\n\r\n* Remove other dated code\r\n\r\n* Fixed convergence and added test for B738_sizing example\r\n\r\n* Add back CODEOWNERS file\r\n\r\n* Inconsequential rendition thump\r\n\r\n* Removed old B738 sizing data\r\n\r\n* Ran black\r\n\r\n* Fix most flake8 errors\r\n\r\n* Fixed ascii art\r\n\r\n* Try to fix remaining flake8\r\n\r\n* Indentation fix\r\n\r\n* Documentation for new components\r\n\r\n* Fixed some errors I noticed in the documentation\r\n\r\n* Address most comments\r\n\r\n* Upper bound on OpenMDAO version\r\n\r\n* Forgot a comma\r\n\r\n* Oldest OpenMDAO version was being overridden on OpenConcept install\r\n\r\n* Try OM 3.16\r\n\r\n* Try OM 3.17\r\n\r\n* 3.17 it is\r\n\r\n* Bump again to 3.21 to fix spline shape problem\r\n\r\n* Add code for checking against OAS and weighted avg of cos(sweep) rather than sweep 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