PANUKL Help - ITLiMS
PANUKL Help - ITLiMS PANUKL Help - ITLiMS
Setting Description Range of panel’s indices used for pressure calculation X coordinate’s range used for pressure calculation X component of pressure taken into account for pitching moment calculation Calculation metod (0-8) Averaging of local coordinate system The values are the numbers of the first and the last panel which will be taken into account for pressure computations. X coordinate’s range used for pressure calculation (global aerodynamic coefficients). X component of pressure taken into account for pitching moment calculation. Computation method selection: 0 – average from two out four of described below methods, 1 – collocation method – with polynomial: φ(x,y)=Ax 2 y 2 +Bx 2 y+Cxy 2 +Dxy+Ex 2 +Fy 2 +Gx+Hy+I, 2 – collocation method (omitting point on current panel) – with polynomial: φ(x,y)=Bx 2 y+Cxy 2 +Dxy+Ex 2 +Fy 2 +Gx+Hy+I, 3 – approximation with polynomial: φ(x,y)=Bx 2 y+Cxy 2 +Dxy+Ex 2 +Fy 2 +Gx+Hy+I, 4 – approximation with polynomial: φ(x,y)=Dxy+Ex 2 +Fy 2 +Gx+Hy+I, 5 – method 1, 2 i 3, 6 – method 1, 2 i 4, 7 – method 1, 3 i 4, 8 – (default) method 2, 3 i 4. Averaging of local coordinate system to eliminate errors during potential differentiation. 40
Downwash calculation: Number of mesh points for downwash calculation longwise Y (X) axis: Number of mesh points for downwash calculation longwise Z axis: X (Y) coordinate of plane for downwash calculation: Y (X) boundary coordinates of downwash mesh: Z boundary coordinates of downwash mesh: Downwash (angle of deviation) computations: None – downwash is not computed (result *.eps file is not created), YZ plane – downwash results are computed in OYZ plane, XZ plane – downwash results are computed in OXZ plane, Number of mesh points for downwash calculation longwise Y (X) axis. Number of mesh points for downwash calculation longwise Z axis. X (Y) coordinate of plane for downwash calculation. Y (X) boundary coordinates of downwash mesh. Z boundary coordinates of downwash mesh. Drag In the Trefz plane Drag in the Trefz plane computation Compressible correction: Compressible correction method for set Mach number: None – no correction, Prandtl-Glauert – correction method Karmana-Tsiena – correction method Function Description Connect two grids Correct neighbours Click to run PANUKL’s application feature which enables user to connect input grids, [4.1]. Click to run program function for correcting neighbours (Fig. 36) for current *.dat (grid & wake) file [4.2]. 41
- Page 1 and 2: Version ENGV1 Warsaw, 01-04-2010 1
- Page 3 and 4: 3.3. Data flow In PANUKL during the
- Page 5 and 6: 1.1.2. Introduction The develop of
- Page 7 and 8: Fig. 1 - Approximation of the body
- Page 9 and 10: - lift force - drag force The aerod
- Page 11 and 12: 1.2.3. Main computational subprogra
- Page 13 and 14: File [name.f] - fuselage geometry -
- Page 15 and 16: File [name.ms2] - complete aircraft
- Page 17 and 18: ottom # key word „bottom” or
- Page 19 and 20: Fig. 6 - The example of „independ
- Page 21 and 22: File [name.TXT] The results for pre
- Page 23 and 24: File [name.CZY] Aerodynamic coeffic
- Page 25 and 26: Fig. 13 - Destination Folder select
- Page 27 and 28: 2.2. PANUKL installation guide in L
- Page 29 and 30: Available options in FILE menu) Fun
- Page 31 and 32: 3.1.2. DRAW menu description Availa
- Page 33 and 34: Fig. 28 - Creating grid file for cu
- Page 35 and 36: Trailing edge angle [deg] Neighbour
- Page 37 and 38: Fig. 32 - Creating *.pan file Fig.
- Page 39: Fig. 34 - Creating output result fi
- Page 43 and 44: Fig. 38 - External XFOIL program wi
- Page 45 and 46: Fig. 41 - Selecting result file wit
- Page 47 and 48: 3.1.6. TOOLS menu description Avail
- Page 49 and 50: Fig. 48 - Graphic representation of
- Page 51 and 52: 3.2. Computational procedure - diag
- Page 53 and 54: 3.3. Data flow In PANUKL during the
- Page 55 and 56: How it Works ? Option 1 - we do hav
- Page 57 and 58: 4.2. Creation of complex computatio
- Page 59 and 60: Step 4 Right side of the object is
- Page 61 and 62: Important notes: What we should kno
- Page 63 and 64: Main program options: Folder path f
- Page 65 and 66: 4.4. How to export geometry from UG
- Page 67 and 68: Remember: don’t insert DATUM PLAN
- Page 69 and 70: In some fuselage areas you will hav
- Page 71 and 72: Fig. 86 - Models prepared with the
Downwash calculation:<br />
Number of mesh points for<br />
downwash calculation<br />
longwise Y (X) axis:<br />
Number of mesh points for<br />
downwash calculation<br />
longwise Z axis:<br />
X (Y) coordinate of plane for<br />
downwash calculation:<br />
Y (X) boundary coordinates of<br />
downwash mesh:<br />
Z boundary coordinates of<br />
downwash mesh:<br />
Downwash (angle of deviation) computations:<br />
None – downwash is not computed<br />
(result *.eps file is not created),<br />
YZ plane – downwash results are computed in OYZ plane,<br />
XZ plane – downwash results are computed in OXZ plane,<br />
Number of mesh points for downwash calculation<br />
longwise Y (X) axis.<br />
Number of mesh points for downwash calculation<br />
longwise Z axis.<br />
X (Y) coordinate of plane for downwash calculation.<br />
Y (X) boundary coordinates of downwash mesh.<br />
Z boundary coordinates of downwash mesh.<br />
Drag In the Trefz plane Drag in the Trefz plane computation<br />
Compressible correction:<br />
Compressible correction method for set Mach number:<br />
None – no correction,<br />
Prandtl-Glauert – correction method<br />
Karmana-Tsiena – correction method<br />
Function Description<br />
Connect two grids<br />
Correct neighbours<br />
Click to run <strong>PANUKL</strong>’s application feature which enables user to<br />
connect input grids, [4.1].<br />
Click to run program function for correcting neighbours (Fig. 36)<br />
for current *.dat (grid & wake) file [4.2].<br />
41
Change language