PANUKL Help - ITLiMS

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3.1.3. DATA menu description Fig. 26 – DATA menu In DATA menu user can find subprograms that are part of the PANUKL application. Now there is only one subprogram FUSELAGE DATA which can help to create fuselage geometry file [name.f]. For more information on FUSELAGE DATA go to chapter 4.2. 3.1.4. CREATE menu description Fig. 27 – CREATE menu CREATE menu is the most important menu in PANUKL. User can perform the complete computational session with functions from CREATE menu for current analyzed object (aircraft). Available options in CREATE menu) Function Description Create grid file This command will run Mesh.exe, PANUKL application component. User will be asked to point input file (complete aircraft geometry file*.ms2). Based on input file the output *.inp, geometry gird file will be created, Fig. 28. 32
Fig. 28 – Creating grid file for current input geometry data Function Description Create grid file with the neighbours This command will run Neigh.exe, PANUKL application component. User will be asked to point input grid file (*.inp). Based on input geometry file the output *.dat, gird with wake file will be created, Fig. 29. The *.dat file contains information about grid, wake and numbers of „neighbours” for current grid panels. Option No. 1 – we do have saved on disk configuration file *.ngh, Fig. 29 Run Create grid file with the neighbours and select saved configuration file *.ngh – file contains all necessary information to create *.dat file. To open selected *.ngh file click OPEN button. Configuration window will appear (Fig. 30) where one can see saved *.dat file creation options. To generate *.dat file click Save and Compute (ok) button. Option No. 2 – we do not have saved on disk configuration file *.ngh, Fig. 29 Run Create grid file with the neighbours and click CANCEL button when prompted for saved configuration file *.ngh. The configuration window will appear (Fig. 30) where user can select options to create *.dat file. To save current *.dat options to *.ngh file click Save [*.ngh] file as, to create *.dat file click Save and Compute (ok) button. 33
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: 3.1.2. DRAW menu description Availa
Page 35 and 36: Trailing edge angle [deg] Neighbour
Page 37 and 38: Fig. 32 - Creating *.pan file Fig.
Page 39 and 40: Fig. 34 - Creating output result fi
Page 41 and 42: Downwash calculation: Number of mes
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

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