OPTIMIZER+Namelist+Input+Parameters

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OPT_METHOD
Selects the mode of operation for Jetstream
 * //Description://**

String
 * //Parameter Type://**

flowsolve, optimize, jacobian, test_prec, chk_metrics, verifyorder, fluxbalance, test_viscjac, adjsolve, extract_geom, mesh_move, design_sweep, mesh_resize, dirderiv,........and the list goes on,........ (See jetstream.f90 for the full list)
 * //Range of Acceptable values://**

none
 * //Default Value://**

JTSTRM% SNOPT_VIOLATION_LIMIT
Defines an absolute limit on the magnitude of the maximum constraint violation after the linesearch. See for details.
 * //Description://**

Double precision
 * //Parameter Type://**

0.0 to +1e20
 * //Range of Acceptable values://**

+1e6
 * //Default Value://**

JTSTRM% USE_IPOPT
Allows the use of IPOPT optimization algorithm instead of SNOPT. See documentation for IPOPT at []
 * //Description://**

Logical
 * //Parameter Type://**

.true. or .false.
 * //Range of Acceptable values://**

.false.
 * //Default Value://**

JTSTRM% secAreaCon
Sectional area constraints to be used for aerodynamic shape optimization problems. Coded as inequality constraints such that wing sectional areas at prescribed spanwise locations must be greater than or equal to target sectional areas. Spanwise locations and corresponding target sectional areas are defined in an input file named //secAreaCons.dat//. When using sectional area constraints, an output file with suffix //.sacon// contains a history of sectional areas at each design iteration. See Jetstream Test Suite case 033 for an example optimization that uses sectional area constraints.
 * //Description://**

Logical
 * //Parameter Type://**

.true. or .false.
 * //Range of Acceptable values://**

.false.
 * //Default Value://**

JTSTRM% NEW_PARAM2

 * //Description://**


 * //Parameter Type://**


 * //Range of Acceptable values://**


 * //Default Value://**