PANUKL Help - ITLiMS

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2. Installation process PANUKL software is made for PCs with Microsoft – Windows 2000/ Windows XP/ Windows Vista software. Additionally it will work on Linux based platforms. Before installation process user must download the latest version of PANUKL software suitable for current operating system. For latest version of program go to: http://itlims.meil.pw.edu.pl/zsis/pomoce/PANUKL/panukl.htm - Files to download – card. 2.1. PANUKL installation guide In MS WINDOWS Step 1) Download the: Panukl_Setup.zip archive file and unpack its content to a free folder on your hard drive. Step 2) Run: Panukl_Setup.exe – The installation window appears Fig. 12. Fig. 12 – Installation Welcome window Step 3) Click NEXT button and choose the destination folder for PANUKL software to install to. The default setting is C:\Program Files\Panukl. Click BROWSE button to change the default installation folder Fig. 13. Click CANCEL button to stop installation. To go to previous installation window click BACK. 24
Fig. 13 – Destination Folder selection Step 4) In next installation setup window, user can select the PANUKL software components to install (or not) Fig. 14. XFOIL and FUSELAGE components are not essential to run PANUKL. Fig. 14 – Select components window Step 5) In next installation setup window user is asked to select Start Menu folder for program’s shortcuts. Additionally one can choose program’s start icon to create on Desktop and in Quick Launch Bar Fig. 15. 25
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: File [name.CZY] Aerodynamic coeffic
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 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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