[UFIG] Result Diagram Screenshot

POST {{hosturl}}/VIEW/CAPTURE

Introduce Input Data Symbols

API - Value Type		Input Data
Integer	🇮	🔴	Essential
String	🇸	❌	Unnecessary
Boolean	🇧	🔺	Optional
Real	🇷

The required Input Data for defining Screenshot setting

NO.	Name	API - Key	API - Value Type	Default	Result Diagram
1	Image Capture Setting	"UFIG_LIST"			🔴
	General Option
2	Perform Analysis Option	"RUN_ANALYSIS"	??	FALSE	🔺
3	Image File Save Path & file name	"OUTPUT_PATH"	🇸		🔴
4	Select Mode before Analysis : true After Analysis : false	"IS_PRE_MODE"	🇧	FALSE	🔺
5	Hidden option	"HIDDEN"	🇧	FALSE	🔺
	Angle of View
6	Horizontal	"VIEW_HORIZONTAL"	🇷	0	🔺
7	Vertical	"VIEW_VERTICAL"	🇷	0	🔺
	Select Load Case
8	Min/Max Case All : “ALL” Max : “MAX” Min : “MIN”	"LOADCASE_MINMAX"	🇸		🔴
9	Load Case Type Static Load Case : “ST” General Comb : “CB” Concrete Comb. “CBC” Steel Comb. : “CBS”	"LOADCASE_TYPE"	🇸		🔴
10	Load Case Name	"LOADCASE_NAME"	🇸		🔴
	Result Diagtam Display Option
11	Result Mode Beam Force Diagram : 6	"CURRENTMODE"	🇮		🔴
	Result Mode Name	"CURRENTMODE_NAME"			🔺
12	Component Axial (Fx) : 0 Shear-y (Fy) : 1 Shear-z (Fz) : 2 TORSION (Mx) : 3 MOMENT-y (My) : 4 MOMENT-z (Mz) : 5 SHEAR-y,z (Fyz) : 9 MOMENT-y,z (Myz) : 10	"RESULT_COMP"	🇮		🔴
13		"POST_DISP_OPT"			🔴
14	Value Display	"PRINT_VALUE"	🇧		🔴
15	Exponential Form	"PRINT_VALUE_EXP"	🇧	FALSE	🔺
16	Value Decimal Point	"VALUE_DECIMAL_PT"	🇮		🔴
17	Legend Display	"PRINT_LEGEND"	🇧		🔴
18	Exponential Form	"PRINT_LEGEND_EXP"	🇧	FALSE	🔺
19	Legend Decimal Point	"LEGEND_DECIMAL_PT"	🇮		🔴
	Value Output Detailes
20	MinMax Only Option	"VALUE_MINMAX_ONLY"	🇧		🔺
21	MinMax Type Min & Max : “MIN MAX” Abs Max : “ABS MAX” Max : “MAX” Min : “MIN”	"VALUE_MINMAX_ONLY_TYPE"	🇸		🔺
22	Limit Scale (%) 0~100	"VALUE_LIMIT_SCALE"	🇮		🔺
23	Set Orientation multiples of 15	"VALUE_ORIENTATION"	🇮		🔺

Result Mode ("CURRENTMODE")

"CURRENTMODE"

No	"CURRENTMODE_NAME"	"CURRENTMODE"
	Reactions
1	REACTION FORCES/MOMENTS	17
	Deformations
2	DEFORMED SHAPE	1
3	DISPLACEMENT CONTOUR	2
	Beam Element
4	BEAM FORCES/MOMENTS	4
5	BEAM DIAGRAMS	6
6	BEAM STRESSES	11
7	BEAM STRESSES DIAGRAM	80
8	BEAM STRESSES(EQUIVALENT)	112
9	BEAM STRESSES(PSC)	76
	Plate Element
10	PLATE FORCES/MOMENTS	9
11	PLANE-STRESS/PLATE STRESSES	12
12	PLANE STRAIN STRESSES	13
	Solid Element
13	SOLID STRESSES	15
	Truss Element
14	TRUSS FORCES	3
15	TRUSS STRESSES	10
	Mode Shapes
16	VIBRATION MODE SHAPES	18
17	BUCKLING MODE SHAPES	19
18	NODAL RESULTS OF RS	86
	Time History Analysis
19	TIME HISTORY DISPL/VEL/ACCEL	61
20	TIME HISTORY FORCES	77
21	TIME HISTORY FORCES DIAGRAM	78

Component ("RESULT_COMP")

Reaction Forces/ Moments

NO	COMPONENT	"RESULT_COMP"
1	FX	0
2	FY	1
3	FZ	2
4	FXYZ	3
5	MX	4
6	MY	5
7	MZ	6
8	MXYZ	7
9	Mb	8
10	Local (if defined)

Deformed Shape & Displacement Contour

NO	COMPONENT	"RESULT_COMP"
1	DX	0
2	DY	1
3	DZ	2
4	DXY	8
5	DYZ	9
6	DXZ	10
7	DXYZ	3
8	Local (if defined)
	Displacement Contour ~~only~~ (Displacement Shape 에서도 제품에는 없으나 아래 번호가 동작함)
9	RX	4
10	RY	5
11	RX	6
12	RW	7

Truss Forces & Truss Stresses

NO	COMPONENT	"RESULT_COMP"
1	All	0
2	Tens.	1
3	Comp.	2

Beam Forces / Moments & Beam Diagrams

NO	COMPONENT	"RESULT_COMP"
1	Fx	0
2	Fy	1
3	Fz	2
4	Mx	3
5	My	4
6	Mz	5
7	Mb	6
8	Mt	7
9	Mw	8
	Beam Diagrams only
10	Fyz	9
11	Myz	10

Plate Forces / Moments

NO	COMPONENT	SUB_COMP. (1)	"RESULT_COMP"	"RESULT_COMP_SUB"
1	Fxx		0
2	Fyy		1
3	Fxy		2
4	Fmax		3
5	Fmin		4
6	FMax		14
7	Mxx		6
8	Myy		7
9	Mxy		8
10	Mmax		9
11	Mmin		10
12	MMax		15
13	Vxx		12
14	Vyy		13
15	Vmax		16
16	Wood Armer Moment		17	WoodArmer 정보 추가 필요
17	Fvector or Mvector	Positive	5 or 11	bVectorPositive 추가 필요
		Negative	5 or 11	bVectorNegative 추가 필요
		Length	5 or 11	dScFactor 작업 필요
		Thickness	UFIG 동작 X

Beam Stresses & Beam Stresses Diagram

NO	COMPONENT	SUB_COMP. (1)	"RESULT_COMP"	"RESULT_COMP_SUB"
1	Sax		0
2	Say		1
3	Saz		2
4	Sby		3
5	Sbz		4
6	Combined	Maximum	5	0
		1 (-y , +z)	5	1
		2 (+y , +z)	5	2
		3 (+y , -z)	5	3
		4 (-y , -z)	5	4

Beam Stresses (Equivalent)

NO	COMPONENT	SUB_COMP. (1)	"RESULT_COMP"	"RESULT_COMP_SUB"
1	Normal		0
2	Tau_xy		1
3	Tau_xz		2
4	Von-Mises		3
5	Max-Shear		4
6	Princ. (max)		5
7	Princ. (min)		6
1-1	Position	Maximum		8
1-2		1 (-y, +z)		0
1-3		2 (+y, +z)		1
1-4		3 (+y, -z)		2
1-5		4 (-y, -z)		3
1-6		5 (N.A, -y)		4
1-7		6 (N.A, +y)		5
1-8		7 (N.A, -z)		6
1-9		8 (N.A, +z)		7

Beam Stresses (PSC)

NO	COMPONENT	SUB_COMP. (1)	SUB_COMP. (2)	"RESULT_COMP"	"RESULT_COMP_SUB"
1	Position 1				0
2	Position 2				1
3	Position 3				2
4	Position 4				3
5	Position 5				4
6	Position 6				5
7	Position 7				6
8	Position 8				7
9	Position 9				8
10	Position 10				9
11	Position 11				10
12	Position 12				11
13	Position 13				12
14	Position 14				13
15	Position 15				14
16	Position 16				15
17	Max				16
18	Min				17
19	Max/Min				18
20	Abs Max				19
1-1	Components	Sig-xx(Axial)		0
1-2		Sig-xx(Moment-y)		1
1-3		Sig-xx(Moment-z)		2
1-4		Sig-xx(Bar)		3
1-5		Sig-xx(Summation)		4
1-6		Sig-zz		5
1-7		Sig-xz(shear)		6
1-8		Sig-xz(torsion)		7
1-9		Sig-xz(bar)		8
1-10		Sig-Is(shear)		9
1-11		Sig-Is(shear+torsion)		10
1-12		Sig-Ps1		11
1-13		Sig-Ps2		12
1-14		7th DOF	Sax(Warping)
			Ssy(Mt)
			Ssy(Mw)
			Ssz(Mt)
			Ssz(Mw)
			Combined(Ssy)
			Combined(Ssz)

Plane-Stress/Plate Stresses

NO	COMPONENT	SUB_COMP. (1)	SUB_COMP. (2)	"RESULT_COMP"	"RESULT_COMP_SUB"
1	Local
1-1	Componenets	Sig-xx		10
1-2		Sig-yy		11
1-3		Sig-xy		12
1-4		Vector	Positive	13	bVectorPositive 작업 필요
			Negative	13	bVectorNegative 작업 필요
			Length	13	dScFactor 작업 필요
			Thickness	동작 X
2	UCS
2-1	Componenets	Sig-xx		0
2-2		Sig-yy		1
2-3		Sig-zz		2
2-4		Sig-xy		3
2-5		Sig-yz		4
2-6		Sig-xz		5
2-7		Sig-max		6
2-8		Sig-min		7
2-9		Sig-eff		8
2-10		Max-Shear		9
3	Element			개발 필요
4	Avg. Nodal	Avg. Nodal Active Only		개발 필요
5	Top			개발 필요
6	Bottom			개발 필요
7	Both Side			개발 필요
8	Abs Max			개발 필요

Vibration Mode Shape & Buckling Mode Shape

NO	COMPONENT	"RESULT_COMP"
1	Md-X	0
2	Md-Y	1
3	Md-Z	2
4	Md-XY	8
5	Md-YZ	9
6	Md-XZ	10
7	Md-XYZ	3
Result for Rotations (API only) 아래는 제품에서 볼 수 없고, 해석결과와 매치해봤을 때 아래와 같을 것이다라는 추론결과입니다.
	Rd-X	4
	Rd-Y	5
	Rd-Z	6

이 위까지 썼습니다 추가 작성 필요..!!!

Plane Strain Stresses / Axisymmetirc Stress

NO	COMPONENT	SUB_COMP. (1)	SUB_COMP. (2)	"RESULT_COMP"	"RESULT_COMP_SUB"
1	Local
1-1	Componenets	Sig-xx		10
1-2		Sig-yy		11
1-3		Sig-xy		12
1-7		Vector	Positive	13	bVectorPositive 작업 필요
			Negative	13	bVectorNegative 작업 필요
			Length	13	dScFactor 작업 필요
			Thickness	동작 X
2	UCS
2-1	Componenets	Sig-xx		0
2-2		Sig-yy		1
2-3		Sig-zz		2
2-4		Sig-xy		3
2-5		Sig-yz		4
2-6		Sig-xz		5
2-7		Sig-max		6
2-8		Sig-min		7
2-9		Sig-eff		8
2-10		Max-Shear		9
2-11		Sig-p1
2-12		Sig-p2
2-13		Sig-p3
2-14		Sig-pmax
3	Element
4	Avg. Nodal	Avg. Nodal Active Only
	Plane-Stress/Plate Stresses only
5	Top
6	Bottom
7	Both Side
8	Abs Max

Nodal Result of RS

NO	COMPONENT	SUB_COMP. (1)
1	Initial Force
1-1	Components	FX
1-2		FY
1-3		FZ
1-4		MX
1-5		NY
1-6		MZ
1-7		Mb
1-8		FXY
1-9		FYZ
1-10		FXZ
1-11		FXYZ
2	Acceleration
2-1	Components	DX
2-2		DY
2-3		DZ
2-4		RX
2-5		RY
2-6		RZ
2-7		RW
2-8		DXY
2-9		DYZ
2-10		DXZ
2-11		DXYZ
3	Mode

Time History Results - Displ/Vel/Accel & Force & Force Diagram

NO	COMPONENT	SUB_COMP. (1)
1	Function
2	TH Load Case Name
3	Step
4	Time Function
5	Displ.
6	Vel.
7	Accel.
	Displ/Vel/Accel
1-1	Components	DX
1-2		DY
1-3		DZ
1-4		DXY
1-5		DYZ
1-6		DXZ
1-7		DXYZ
	Time History Force & Force Diagram
2-1	Components	Fx
2-2		Fy
2-3		Fz
2-4		Mx
2-5		My
2-6		Mz

The JSON format example for inputting Screenshot setting

API EXAMPLE - Screenshot setting - Result Diagram

{
  "Argument": {
    "UFIG_LIST" : [
        {
            "OUTPUT_PATH" : "C:\\MIDAS\\Image\\Diagram1.jpg" ,
            "IS_PRE_MODE" :  false,

            "VIEW_HORIZONTAL" : 0,
            "VIEW_VERTICAL" : 0,

            "LOADCASE_MINMAX" : "ALL",
            "LOADCASE_TYPE" : "CB",
            "LOADCASE_NAME" : "LCB1",

            "CURRENTMODE" : 6,
            "RESULT_COMP" : 10,
            "POST_DISP_OPT" : 
            {
                "PRINT_VALUE" : true,
                "VALUE_DECIMAL_PT" : 3,
                "PRINT_LEGEND" : true,
                "LEGEND_DECIMAL_PT" : 3
            }
        }
    ]
  }
}