FLZ-Vortex-Help
Table of Content:
1: Introduction
2: Limitations in
DEMO-Version
3: Licence
4: Installing FLZ-Vortex
5: Getting started
6.1: File
6.2: Preferences /
Directories
6.3: Preferences / Colours
6.4: Preferences / Redo-
Undo-Files
6.4.1: Change Marking-bar
to Cross
6.5: Languages
6.6: Help
6.7: Formula Symbols
7: Folder Airplane / Input
field current Airplane
7.1: Generate New
Airplane
7.2: Input Designer's Name and Identifier of
Airplane
7.3: Position of Airplane in Virtual Room
7.4: Viewing Angle of Airplane in Virtual Room
7.5: Additional Masses
7.6: Zero-Point Offset
7.7: Scaling / Change Size of whole Airplane
8: Folder Wing / Input field Wing Root
8.1: Creating a new Wing
8.2: Input Designation of Wing
8.3: Positioning the Wing
8.4: Number of Panels X
8.5: Distribution of Panels in X-direction
8.5.1: Optimization of Airfoil Zero-Coefficients
8.5.2: Input Resolution of Panels in Solid modelling
8.6: Input of Chord line
8.7: Input Mass of Wing
8.8: Input Angle of Incident
8.9: Select Root-Airfoil
8.10: Select actual Wing
8.11: Copy a Wing
8.12: Import Flying Wing FLG-File
8.13: Delete current Wing
8.14: Input Angle for Geometric Twist
8.15: Generating an
elliptic Wing
9: Folder Wing / Input field Segment
9.1: Select actual Segment
9.2: Change Width of Segment
9.3: Input Chord line of Airfoil
9.4: Input Dihedral Angle
9.5: Input Sweep
9.6: Input Angle for Geometric Twist
9.7: Input Number of Panels Y
9.8: Distribution Y
9.9: Create new Segments
9.10: Delete Segment
9.11: Split Segment
9.12: Edit Flaps / Adjustment
9.13: Select Segment Airfoil
10: Folder Wing / Input field Half-Wing
11: List of Surfaces / Quick Selection / Switching Surface
visible-invisible
12: Folder 3D / Graphic buttons
12.1: Rotate Airplane
12.2: Shift Airplane
12.3: Zoom Airplane
12.4: Edit Airplane
12.5: Hidden Lines
12.6: Display Bound Vortices
12.7: Filled Panels / Lattice Graphics
12.8: Display Free Vortices (wake turbulence)
12.9: Mark Segment Edges
12.10: Display Panel normal vector
12.11: Draw Angle of Incident
12.12: Display 3D-Model
12.13: Draw Moment Rotation Direction
12.14: Draw Zero-Point of airplane
12.15: Change Length of Auxiliary Lines
12.16: Display Panel Force Vector
14.1: Angle of Attack
14.2: Lift Coefficient Cl
14.3: Stability Measure
14.4: Centre of Gravity
14.5: Airspeed
14.6: Start / Stop Computation
14.7: Sideslip Angle
14.8: Altitude
14.9: Wake Turbulence
14.10: Computed Values
14.11: Input additional Drag
15:
Folder 2D and Display of Curves
15.1: Display current Wings
15.2: Display CP, CG and NP
15.3: Display Strength of Circulation (Gamma)
15.4: Display Distribution of Cl
15.5: Display Distribution of Cdi
15.6: Display Distribution of ai
15.7: Display Distribution of Reynolds Number
15.8: Airfoil Cross-Section
15.9: Display Contour of whole Airplane
15.10: Output of Flap Angle
15.11: Positioning the Marking-bar
17:
Folder Total-Polars Computation
17.1: Flap Computations
17.2: Angle of Incidence Computation
17.3: Viewing Polars as Table or Graphic
19.1: Formatted
Geometry-Export
19.2: Formatted Export, Computed Values
19.3: Formatted Export Polars