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3 Jan 2008: group 6 6 extrras 9-4-03 Reference Area : 0.0675 mm Reference Length : 0.1500 m Atmos. Pressure : 101.6000 KPa Ref. Temperature : 23.60 Deg C Ref. Density : 1.1936 Kg/(mmm) D L PM Ai DP Cd Cl Cm V group 6 6 extrras 9-4-03 Reference Area : 0.0675 mm

3 Jan 2008: Group 5 2-4-03 Reference Area : 0.0900 mm Reference Length : 0.1500 m Atmos. Pressure : 101.9000 KPa Ref. Temperature : 23.90 Deg C Ref. Density : 1.1959 Kg/(mmm) D L PM Ai DP Cd Cl Cm V Group 5 2-4-03 Reference Area : 0.0900 mm Reference Length :

3 Jan 2008: group 1,2,3,4 AERO3260 5-8-05 Reference Area : 0.1800 mm Reference Length : 0.1500 m Atmos. Pressure : 102.4000 KPa Ref. Temperature : 15.10 Deg C Ref. Density : 1.2385 Kg/(mmm) Balance Sensitivity Settings : D CWF L RM PM YM Ai ASS DP 3.0E0001

3 Jan 2008: group4 Reference Area : 0.1273 mm Reference Length : 0.2120 m Atmos. Pressure : 102.0560 KPa Ref. Temperature : 19.30 Deg C Ref. Density : 1.2166 Kg/(mmm) D CWF L RM PM YM Ai ASS DP Cd Ccwf Cl Crm Cpm Cym V group4 Reference Area : 0.1273 mm

3 Jan 2008: 1998 sweep angle 10o Reference Area : 0.0910 mm Reference Length : 0.1520 m Atmos. Pressure : 103.4700 KPa Ref. Temperature : 17.80 Deg C Ref. Density : 1.2398 Kg/(mmm) D CWF L RM PM YM Ai ASS DP Cd Ccwf Cl Crm Cpm Cym V 1998 sweep angle 10o

3 Jan 2008: failed lastweek grop X 28-4-04 Reference Area : 0.0960 mm Reference Length : 0.1600 m Atmos. Pressure : 102.3700 KPa Ref. Temperature : 20.40 Deg C Ref. Density : 1.2158 Kg/(mmm) D L PM Ai DP Cd Cl Cm V failed lastweek grop X 28-4-04 Reference Area :

3 Jan 2008: group 8 27-4-2004 Reference Area : 1.0000 mm Reference Length : 1.0000 m Atmos. Pressure : 101.3000 KPa Ref. Temperature : 15.00 Deg C Ref. Density : 1.2256 Kg/(mmm) D L PM Ai DP Cd Cl Cm V group 8 27-4-2004 Reference Area : 1.0000 mm Reference

3 Jan 2008: grp3,19/8/99, Reference Area : 0.1272 mm Reference Length : 0.2120 m Atmos. Pressure : 101.8000 KPa Ref. Temperature : 19.40 Deg C Ref. Density : 1.2131 Kg/(mmm) D CWF L RM PM YM Ai ASS DP Cd Ccwf Cl Crm Cpm Cym V grp3,19/8/99, Reference Area :

3 Jan 2008: 60 degree sweep back group 18 23-4-2004 234456778 Reference Area : 1.0000 mm Reference Length : 1.0000 m Atmos. Pressure : 101.3000 KPa Ref. Temperature : 15.00 Deg C Ref. Density : 1.2256 Kg/(mmm) D L PM Ai DP Cd Cl Cm V 60 degree sweep back group

3 Jan 2008: group x 22-apr-2004 11.00 Reference Area : 1.0000 mm Reference Length : 1.0000 m Atmos. Pressure : 101.3000 KPa Ref. Temperature : 15.00 Deg C Ref. Density : 1.2256 Kg/(mmm) D L PM Ai DP Cd Cl Cm V group x 22-apr-2004 11.00 Reference Area : 1.0000

3 Jan 2008: LAST GROUP! 30-4-2004 Reference Area : 0.0960 mm Reference Length : 0.1600 m Atmos. Pressure : 100.5400 KPa Ref. Temperature : 20.80 Deg C Ref. Density : 1.1924 Kg/(mmm) D L PM Ai DP Cd Cl Cm V LAST GROUP! 30-4-2004 Reference Area : 0.0960 mm

3 Jan 2008: group #@ 23-4-04 Reference Area : 1.0000 mm Reference Length : 1.0000 m Atmos. Pressure : 101.3000 KPa Ref. Temperature : 15.00 Deg C Ref. Density : 1.2256 Kg/(mmm) D L PM Ai DP Cd Cl Cm V group #@ 23-4-04 Reference Area : 0.1020 mm Reference Length

25 Jun 2008: the play button is a good test for conversion. If Ff Play will not play the file, Ffmpeg will not convert it. ... Again, the Play button is a good test. If Ff play will not play the file, Ffmpeg will most likely not convert it.

3 Jan 2008: Figure 4 shows the contentsof the test.ana file. B.2 Netlist the Design. ... PRINT V(OUT);. END;. Figure 4: SWITCAP Analysis File, test.ana. Figure 5: Simulation Results – Sinusoidal Steady State.

29 Jun 2008: Used to test the state of a particular pin. For setting the state of a particular pin. • ... If the test condition doesnot change somehow within the loop, the loop will never terminate.(endless loop).

3 Jan 2008: PROCEDURE. The plate is mounted in the tunnel test section. The probe is mounted on a traverse mechanism attached to the roof of the tunnel. ... The tunnel piezo-electric manometer can be used to calculate the test section flow dynamic pressure and hence

28 Jun 2008: There areimportant differences, most of which cause problems whentrying to build and test PLIB, so these rarely impact Flight-Gear directly. ... ARINC. Todd Moyer of ARINC used FlightGear as part of an effortto test and evaluate Flight Management

3 Jan 2008: stack? 4. Can you devise a simple experiment to verify your calculations, or to do a quick test before you even start the calculations (and spend the time on them?).

3 Jan 2008: gnetlist -g cascade -o test.cas file1.sch [file2.sch. ]. For the example file contained in this archive, you can run:.

3 Jan 2008: Summarize the major risks you might encounter as you build, test, and operate.