13.Design.wing

13.Design.wing - MEM 425: aircraft design & performance...

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MEM 425: aircraft design & performance Wing loading Dr. Ajmal Yousuff Dept. MEM Drexel University
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Estimate of Wing Loading Normally it is take_off wing loading. could use any or all of these: stall speed climb rate landing take_off turns yousuff MEM 425 aircraft design Page 2
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Stall speed V stall is normally given or specified from level flight: yousuff MEM 425 aircraft design Page 3 (about 70-100 mph)
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Take_off distance yousuff MEM 425 aircraft design Page 4 : ( ) ( ) TO TO L L W hp prop C SW WT je to ts C S p W p to    Top:
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Take off parameter (top) Recall: yousuff MEM 425 aircraft design Page 5 max max 2 1.21 1 1.21 LO L SL L W S g SC T W T gS C W
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Balanced field length Distance to decision speed point plus the remaining distance. decision speed : speed @ which the distance to TO & clear obstacle (35’) equals the distance to stop, if one engine fails.
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This note was uploaded on 04/26/2011 for the course MEM 425 taught by Professor Yousuff during the Spring '08 term at Drexel.

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13.Design.wing - MEM 425: aircraft design & performance...

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