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1 Exercise 4: propeller type) aircraft from last week. Selected Aircraft (from last week's module):

Published on November 2017 | Categories: Comics | Downloads: 12 | Comments: 0
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Exercise 4: Drag and ApplicationsThe first part of this week’s assignment is to revisit our reciprocating engine powered (i.e. propeller type) aircraft from last week. 1. Selected Aircraft (from last week’s module):Pilata PC-12Make sure to review your data and results from last week and any feedback that you mayhave received on your work, in order to prevent continuing with faulty data.2. Main Wing Airfoil type & on-line database designator (from last week’s module): NASA/LANGLEY LS(1)-0417MOD AIRFOIL (ls417mod-il)3. Aircraft Maximum Gross Weight [lbs] (from last week’s module):10,450 lbs4. Wing Span [ft] (from last week’s module): 53.3 ft5. Average Chord Length [ft] (from last week’s module):5.23 ft6. Wing Area ‘S’ [ft2] (from last week’s module):277.8 ft ^27. Find the Aspect Ratio ‘AR’ for your selected aircraft wing. (Use the wing span and average chord length from last week’s module/from above. See also page 63 in your textbook.):10.19 ft8. CLmax for your airfoil (from last week’s module): 1.90249. Standard sea level Stall Speed ‘Vs’ for your aircraft [kts] (from last week’s calculation):76.38ktsFind the appropriate drag polar curve for your airfoil selection (2. above; from last week’s module). You can utilize any officially published airfoil diagram for your selected airfoil or use again the Airfoil Tool at http://airfoiltools.com/search

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Exercise 4: Drag and ApplicationsThe first part of this week’s assignment is to revisit our reciprocating engine powered (i.e. propeller type) aircraft from last week. 1. Selected Aircraft (from last week’s module):Pilata PC-12Make sure to review your data and results from last week and any feedback that you mayhave received on your work, in order to prevent continuing with faulty data.2. Main Wing Airfoil type & on-line database designator (from last week’s module): NASA/LANGLEY LS(1)-0417MOD AIRFOIL (ls417mod-il)3. Aircraft Maximum Gross Weight [lbs] (from last week’s module):10,450 lbs4. Wing Span [ft] (from last week’s module): 53.3 ft5. Average Chord Length [ft] (from last week’s module):5.23 ft6. Wing Area ‘S’ [ft2] (from last week’s module):277.8 ft ^27. Find the Aspect Ratio ‘AR’ for your selected aircraft wing. (Use the wing span and average chord length from last week’s module/from above. See also page 63 in your textbook.):10.19 ft8. CLmax for your airfoil (from last week’s module): 1.90249. Standard sea level Stall Speed ‘Vs’ for your aircraft [kts] (from last week’s calculation):76.38ktsFind the appropriate drag polar curve for your airfoil selection (2. above; from last week’s module). You can utilize any officially published airfoil diagram for your selected airfoil or use again the Airfoil Tool at http://airfoiltools.com/search

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