PANUKL Help - ITLiMS

More documents

Recommendations

Info

Fig. 29 – Creating *.dat file (grid with wake) Fig. 30 – Configuration options – creating *.dat file (grid with wake) Setting Description Length of the wake (MAC multiplication) Wake type description Length of the wake (MAC multiplication) Wake type creation methods: 0 – Wake parallel to MAC 1 – Wake with downwash due to angle of attack 34
Trailing edge angle [deg] Neighbour condition angle [deg] 2 – Wake with downwash due to sideslip of attack 3 – Wake parallel to the free stream 4 , 5, 6 – Wake with the same effect as in cases 1-3 but only for last wake panels Trailing edge angle. If the angle between two trailing edge grid panels is lower or equal to defined value, than wake line will be created from such trailing edge. Neighbor condition angle . If the angle between two neighboring grid panels is higher than defined value, both panels are not treated as neighbours. Angle of attack [deg] Angle of attack (taken into account during wake creation). Sideslip angle [deg] Sideslip angle (taken into account during wake creation). Fig. 31 – *.dat file example: grid & wake „Predator.dat” 35
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: Fig. 28 - Creating grid file for cu
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

PANUKL Help - ITLiMS

Create successful ePaper yourself

Delete template?

Save as template?