PANUKL Help - ITLiMS

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3. Working with PANUKL 3.1. PANUKL GUI description To run PANUKL’s GUI, click GridView.exe managing subprogram icon, on the DESKTOP or in the START MENU. After few seconds the main application window displays Fig. 19. PANUKL is ready to operate. Fig. 19 – Main application window To change program window size use standard WINDOWS buttons. User can access the particular program functions from drop down managing application MENU. 3.1.1. FILE menu description Fig. 20 – FILE menu 28
Available options in FILE menu) Function Description Open grid file [Ctrl+O] Open grid file with Wake [Alt+Ctrl+O] Open pressure distribution file [Alt+Ctrl+T] Open grid file *.inp, from user selected disc location, Fig. 21. Open grid file with wake *.dat, from user selected disc location. Open output *.txt file with pressure distribution for current analyzed body (for each grid panel). Open and show results file Open and show global results *.out file in external window, Fig. 23. Save picture as [Ctrl+S] Exit [Alt+X] Save current graphical window to JPEG , PNG or BMP file , Fig. 22. End program, exit application. Fig. 21 – File selection window example File selection Windows can be different dependent on the current operating software version, window looks does not influence PANUKL’s functionality. 29
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: 2.2. PANUKL installation guide in L
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 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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