HW3-1

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Purdue University *

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45400

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Mechanical Engineering

Date

Feb 20, 2024

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pdf

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4

Uploaded by ProfessorUniverseMule20

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ASW Preliminary Sizing 1. Warmup and take-off W1/W TO = 0.97 2. Climb W2/W1= 0.985 nm ft 3. Cruise 01 R= 1500 9114180 1/hr 1/s C= 0.5 0.00013889 M ft/s V= 0.6 596.88 A= 7 Swet/Sref= 5.5 K LD = 14 L/Dmax = 15.79 Lift to drag cruise factor 0.866 L/D = 13.68 W3/W2 = 0.85636847 hr s 4. Loiter 01 E= 3 10800 1/hr 1/s C= 0.4 0.00011111 Lift to drag loiter factor 1 L/D = 15.79 W4/W3 = 0.92683697 5. Cruise 02 (same as 3.) W5/W4 = 0.85636847 min s 6. Loiter 02 E= 20 1200 1/hr 1/s C= 0.4 0.00011111 Lift to drag loiter factor 1 L/D 15.79 W6/W5 = 0.99159358 7. Land W7/W6 = 0.995 Total Fuel Fraction W7/W TO = 0.64075122 FF = 1.06(1-W7/WTO) FF= 0.38080371 ࠵? ࠵? ௠௔௫ = ࠵? ௅஽ ࠵? ࠵? ௪௘௧ ࠵? ௥௘௙ ࠵? ࠵? ௜ିଵ = ࠵? ି ோ஼ ࠵? ࠵? ௜ିଵ = ࠵? ି ா஼ ࠵? ࠵? ௜ିଵ = ࠵? ି ா஼ g1a) Cruise 2-3 range High-bypass Turbofan Mach O for jet engines . 3 has loitering . O-- for jet engines .
W TO = 20129.3451 lb Structure Factor Parameters A = 1.59 C = -0.1 SF (military cargo/bomber) SF = 0.59022032 Payload W PL = 10800 lb Structure Weight Ws = 11880.7486 lb Fuel Weight Wf = 7665.32918 lb Weight Buildup Equation W PL + Ws + Wf 30346.0777 lb Error 10216.7327 ࠵?࠵? = ࠵? ࠵? ்ை = ࠵?࠵? ்ை ࠵? ௩௦
C) Keeping all the other parameters same as a) Only payload weight has been changed to 6600 db because Avionics weight has been changed to 3800db With crew weight as 800db Wa = 6600db WTo = 26 , 146 . 078db . Changing the payload weight to 16600 because Avionic weight is 16800db and crew weight Goodb Wpc = 15800db WTo = 36146 . 078 Ab . d) Composites have reduced the structural weight in 5 %. -118800749db of S % is is 11286 . 71/db 594 . 03743 Ib remaining (similiar params as a) WTo = 29752 . 04 Nb
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Weight_TO (lb) Range (nm) 28857.20371 1000 30346.07773 1500 31688.73468 2000 Weight_TO (lb) Payload (lb) 26146.07773 6600 30346.07773 10800 36146.07773 16600 0 500 1000 1500 2000 2500 28500 29000 29500 30000 30500 31000 31500 32000 Range (nm) Weight (lb) Weight vs range 0 2000 4000 6000 8000 10000 12000 14000 16000 18000 0 5000 10000 15000 20000 25000 30000 35000 40000 Payload (lb) Weight (lb) Weight vs payload