ACJC 9649 2023 Prelim P1 Solutions
Uploaded by toastedbagels · 28 October 2023
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Text from the first pages1 3d 4 d4 , 8dd xy ttt t t 22 3 6 2 2 62 2 62 2 2 3 24 2 2 2 2 d d 4 48dd 1616 32 64 1616 32 116 2 116 16 1 xy ttt t t t t t t tt t tt t t t t t Surface area 4 2 6 2 6 2 1 1 5 1 4 2d 32 d 1232 32 23 1 π4 π 1 1 1ππ 6 2 6 k k k t t tt t tt tt kk Solving 62 π12 3 1π 38 2 4632 k k , we get 2k . Since 1k , 2k . 2 Multiply throughout by 1nn 1 14( 1) 2nn nnn x n x Let n nnn x y , 142nnyy where 1 1y 142ny 2 24 4 2 2ny 32 34 4 2 4 2 2ny 1 2 3 14 4 2 4 2 4 2 2n n ny 1 1 2(1 4 )4 14 n n 11 24 1 4 3 nn
12 5 4 3 n Hence 12 5 4 3 n n nx n . Alternative solution 142nnyy where 1 1y The general solution is of the form 14n n Aky . Let 0k , so 2 342A AA . So the general solution is 12 43 n ny k . Since 1 1y , we have 3 21 34 5k k . Hence 125 433 n ny . 3(a) Let y ux d d dd y uuxxx 2 3 2 3d d yx y x x y yx 32 3 2 d d ux ux u x x x ux uxx 2 3 4 3 3 3 3 d d uu x ux x ux u xx 23d 1d uux u u ux 32 d1 d1 uu xxu u u 2 1dd( 1)( 1) u ux xuu Let 22 11( 1)( 1) ( 1) u A B C uuu u u 2( 1) ( 1)( 1) ( 1)u A u B u u C u Let 1u : 14 A 1 4A Let 1u : 12 C 1 2C Let 0u : 110 42 B 1 4B 2 1 1 1 d ln4( 1) 4( 1) 2( 1) u x cuu u 1 1 1ln 1 ln 1 ln4 4 2( 1)u u x c u 1 1 1ln ln4 1 2( 1) u xcuu
4( 1)11ln4 1 2( 1) xu cuu 4( 1) 2ln 11 xu cuu (where 4cc ) Sub. yu x : 4 1 2ln 11 yx x cyy xx 4() 2ln x y x x cy x y x Since xy , 0yx , so the general solution is 4() 2ln x x y x cy x y x 3(b) 3 2 3 2 d d y x x y y x xy Let 3 2 3 2 22f , 1 x x y y y xxy yx y x , 0 2x , 0 1y . Using Euler method with step size 0.5, 1 0 0 0 2 2 0.5f , 211 0.5 1 1 2 2.375 y y x y 3(c) The approximation is an over-estimate. 4(i) T3det det det ( 1) det det A A A A A since A is skew symmetric Since det det det 0 A A A . 4(ii)(a) Method 1 x y (2, 1) (2.5, 2.375)
ax 11 22 33 ax ax ax 2 3 3 2 3 1 1 3 1 2 2 1 a x a x a x a x a x a x 3 2 1 3 1 2 2 1 3 0 0 0 a a x a a x a a x 32 31 21 0 0 0 aa aa aa M Method 2 1 23 32 10 0 0 a aa aa ai 13 2 31 0 10 0 aa a aa aj 12 21 3 0 0 10 aa aa a ak 32 31 21 0 0 0 aa aa aa M 4(ii)(b) M is skew symmetric and so by (i) det 0 M Hence M is not invertible. 4(ii0(c) ker |T k k a , the set of vectors parallel to a or line through origin and parallel to a 3R( ) | 0T v a v , the set of vectors perpendicular to a or plane through origin and perpendicular to a
5(i) cos cos 2 sin 2 cos sin sin 2 cos 2 sin cos 2 cos sin 2 sin sin 2 cos cos 2 sin cos(2 ) sin(2 ) cos sin T sin cos 2 sin 2 sin cos sin 2 cos 2 cos cos 2 sin sin 2 cos sin 2 sin cos 2 cos sin(2 ) cos(2 ) sin cos T The eigenvalues are 1 and 1 with eigenvector cos sin and sin cos respectively. 5(ii) 110 01 T R R 5(iii) π 3 13 22 31 22 T 13 3122 22 2 11 131 3 222 T 5(iv) TT cos 2 sin 2 cos 2 sin 2 sin 2 cos 2 sin 2 cos 2 cos 2 cos 2 sin 2 sin 2 cos 2 sin 2 sin 2 cos 2 sin 2 cos 2 cos 2 sin 2 sin 2 sin 2 cos 2 cos 2
cos 2( ) sin 2( ) sin 2( ) cos 2( ) which is a rotation through an angle of 2( ) 6(i) 2 1f ( ) 2xx x 2 11f (2) 2 2 024 2 18f (3) 3 2 039 Since f ( )yx is a continuous curve over the interval 2,3 with f (2) f (3) 0 , therefore there exists a root in the interval. 6(ii) Let 1 2 f (3) 3 f (2) 91 f (3) f (2) 41x Note that 91f0 41 . 912, 41 91 91 41 41 91 41 2 f ( ) f (2) 2.106450495f ( ) f (2) 2.11 (3.s.f) 6(iii) 2 1f ( ) 2xx x 1 2 3 21f ( ) 2 0 2xx x for 912x 41 3 2 4 61f ( ) 2 0 4xx x for 912x 41 2 1f ( ) 2xx x is concave upward and its gradient negative over the interval 912x 41 , is an over - estimate of the root. 6(iv) 2 1f ( ) 2xx x , 3 21f ( ) 22 x x x Applying 1 f ( ) f ( ) n nn n xxx x with 0 2.5x , 0 10 0 f ( ) 1.844866f ( ) xxx x 1 3 11 21f ( ) 22 x xx is undefined for 1 1.84486x . Therefore the Newton-Raphson method failed.
6(v) 1 4 12n n x x 0 3x 1 4 0 12 2.012x x 2 4 1 12 2.061x x 3 4 2 12 2.055x x is 2.06 correct to 3 s.f. Since f (2.055) 0.00227 0 and f (2.065) 0.02044 0 , 2.06 is sufficiently accurate correct to 3 significant figures. 7(i) Volume of revolution about y-axis, V 3π 12 0 2π d a xy x 3π 2 0 d2π ( sin ) (1 cos ) dd xa t t a t t t 3π 22 0 2π ( sin ) (1 cos ) da t t a t t 3π 32 2 0 2π ( sin )(1 cos ) da t t t t (Shown) 7(ii) V 3π 3 2 22 0 2π ( 2 cos cos ) ( sin )(1 cos ) da t t t t t t t t Let cos d sin cosI t t t t t t c ----(1) Let 2cos dJ t t t du 1dut t 2 1 1 1 2 2 4 dv cos (1 cos 2 )d sin 2d t v t t t tt 21 1 1 1 2 4 2 2 sin 2 ( sin 2 )dJ t t t t t t 221 1 1 1 1 2 4 2 2 4 sin 2 cos 2J t t t t t c 21 1 1 1 2 2 2 4 sin 2 cos 2J t t t t c
Let 2( sin )(1 cos ) dK t t t 23 1 3( sin )(1 cos ) d (1 cos )K t t t t c 3π 3 2 22 0 2π ( 2 cos cos ) ( sin )(1 cos ) d V a t t t t t t t t 3π 21 2 2 32 1 1 1 1 2 2 2 4 31 3 0 2( sin cos ) 2π sin 2 cos 2 (1 cos ) t t t t a t t t t t 3π 23 2 4 3 11 48 31 3 0 2 sin 2cos 2π sin 2 cos 2 (1 cos ) t t t t a t t t t 227 16 33 11 88 1 3 π 0 3π 0 2 0 2π 0 2π 0 0 aa 32 27 17 16 122π π 3πa 8(a) d d vm C kvt 1 d 1 d v C kv t m 11 ddvtC kv m 1 ln tC kv ckm (for arbitrary constant c) ln ktC kv kc m C kv e kt kcm e kt mA (where e kcA ) When 0t , 0vv : 0A C kv 0 e kt mC kv C kv 0 e kt mC C kvv k 8(b) As t , e0 kt m , so Cv k .
After a long time, the velocity of the falling body approaches the constant value C k , which is independent of the initial velocity 0v . 8(c)(i) d d vm C qt kvt d d C qtvk vt m m Multiply both sides by integrating factor d ee k kttmm : de e ed kt kt kt m m m C qtvk vt m m de ed kt kt m mv C qttm e kt mv e d kt m C qt tm ee d kt kt mm C qt q tkk e e d kt ktm mqC qt tkk ee kt kt mm q mC qt ck k
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