Q2:A) What are the classifications of the NACA Aerofoil section? B) Select the appropriate NACA airfoil section for the wing, which will use for a civilian category airplane with the following characteristics: MTO=9500 kg, S = 40 m², Vc = 300 m/sec (at 9000m, p-0.4671 kg/m³), Vs = 20 m/sec (at sea level) The high lift device (plain flap) will provide act. -0.5 when deflected. Use the figure below for selecting if it fits, then, discuss your answer. Maximum lift coefficient (Cimer) 45,-018 65,-021 0000 1.5 64,015 64,013 16-01863,-01260,915 66,-021 64,-021 1.3 64,018 1 teas 66,012 0.7 1.3 0.9 0.8 0012 www 63,-015 54-218.653-2 43,018 2455,0. 24 1.1009 64-112 €5.000 164-019 0 1410 0006 66006 GADIO, GEAd10 900-19 0010-34 0010-35 44-110 +8612-45 1.066-09-19. 1408 63-210 95,-212 0.1 44-2184 64-209 63,-211 1412 63,315 0012-644-418 64,-21265215 64A-210 65-210 2410 64-A315 65-221 012-59253 439-409 65-209 0.2 66-206 23013 65-415 S 63,-415 21-211 23012 45-410 255-415 25-01 44,-418 64,-421 3476415 65-418 7476315 2421 33034 L(medin 166-17 64,-411 65,415 64,415 65,412 64M41 0.3 43-421 65,-431 63,318 63-309 64-210 DIEVED 66-211 66,-212 04412 0.4 4415 PELA 2418,2408 All dan at Re of 6x10, and no Dap deflection 4424 0.5 63-613 65,-618 64,-628 63,618 63-618 0.6
Q2:A) What are the classifications of the NACA Aerofoil section? B) Select the appropriate NACA airfoil section for the wing, which will use for a civilian category airplane with the following characteristics: MTO=9500 kg, S = 40 m², Vc = 300 m/sec (at 9000m, p-0.4671 kg/m³), Vs = 20 m/sec (at sea level) The high lift device (plain flap) will provide act. -0.5 when deflected. Use the figure below for selecting if it fits, then, discuss your answer. Maximum lift coefficient (Cimer) 45,-018 65,-021 0000 1.5 64,015 64,013 16-01863,-01260,915 66,-021 64,-021 1.3 64,018 1 teas 66,012 0.7 1.3 0.9 0.8 0012 www 63,-015 54-218.653-2 43,018 2455,0. 24 1.1009 64-112 €5.000 164-019 0 1410 0006 66006 GADIO, GEAd10 900-19 0010-34 0010-35 44-110 +8612-45 1.066-09-19. 1408 63-210 95,-212 0.1 44-2184 64-209 63,-211 1412 63,315 0012-644-418 64,-21265215 64A-210 65-210 2410 64-A315 65-221 012-59253 439-409 65-209 0.2 66-206 23013 65-415 S 63,-415 21-211 23012 45-410 255-415 25-01 44,-418 64,-421 3476415 65-418 7476315 2421 33034 L(medin 166-17 64,-411 65,415 64,415 65,412 64M41 0.3 43-421 65,-431 63,318 63-309 64-210 DIEVED 66-211 66,-212 04412 0.4 4415 PELA 2418,2408 All dan at Re of 6x10, and no Dap deflection 4424 0.5 63-613 65,-618 64,-628 63,618 63-618 0.6
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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