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4.3. FUSELAGE DATA – external subprogram description Program FUSELAGE DATA FUSELAGE DATA program was made to help with creating fuselage/ nacelle geometry files [name.f] for <strong>PANUKL</strong> application. With FUSELAGE DATA we can create: Fuselage geometry file [name.f] from txt [name.w] files. Each file contains frame outline definition points described by free coordinates. Fuselage geometry file [name.f] from txt [name.txt] UNIGRAPHICS files. Each UNIGRAPHICS file contains information about point describing one frame. Important note: Each fuselage or nacelle section/ frame needs one [name.w] or [name.txt] file with points describing its geometry. The section/frame point coordinates order in file is free. Modification of present fuselage files [name.f] Main FUSELAGE DATA application window Fig. 71 – Main FUSELAGE application window 62
Main program options: Folder path for input fuselage geometry frame files: [name.w] or [name.txt] files. Browse button, for input files. Output fuselage geometry file name and path [name.f]. Browse button, for output file. CREATE or MODIFY program modes. Fuselage geometry file – Preview button. Fig. 72 – Fuselage geometry file – preview window Create mode in FUSELAGE DATA Fig. 73 – Create mode in FUSELAGE program 63
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Version ENGV1 Warsaw, 01-04-2010 1
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3.3. Data flow In PANUKL during the
Page 5 and 6:
1.1.2. Introduction The develop of
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Fig. 1 - Approximation of the body
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- 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 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: Important notes: What we should kno
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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