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Solve for x and k. Model 1: log2(x) + 4 logx(8) = 8. Model 2: 3^(2k+1) - 28 3^k + 9 = 0

Mathematics

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  1. Find the larger value of the fuel flow rate xx using Model 1.

    Model 1: log⁡2x+4log⁡x8=8\log_2 x + 4 \log_x 8 = 8
    First, change the base of log⁡x8\log_x 8 to base 2 using the change of base formula log⁡ba=log⁡calog⁡cb\log_b a = \frac{\log_c a}{\log_c b}:

    log⁡x8=log⁡28log⁡2x=3log⁡2x\log_x 8 = \frac{\log_2 8}{\log_2 x} = \frac{3}{\log_2 x}

    Substitute this into the equation:

    log⁡2x+4(3log⁡2x)=8\log_2 x + 4 \left(\frac{3}{\log_2 x}\right) = 8 log⁡2x+12log⁡2x=8\log_2 x + \frac{12}{\log_2 x} = 8

    Let u=log⁡2xu = \log_2 x. The equation becomes:

    u+12u=8u + \frac{12}{u} = 8

    Multiply by uu:

    u2+12=8uu^2 + 12 = 8u

    Rearrange into a quadratic equation:

    u2−8u+12=0u^2 - 8u + 12 = 0

    Factor the quadratic equation:

    (u−2)(u−6)=0(u-2)(u-6) = 0

    This gives two possible values for uu: u=2u=2 or u=6u=6.
    Substitute back u=log⁡2xu = \log_2 x:
    If u=2u=2, then log⁡2x=2  ⟹  x=22=4\log_2 x = 2 \implies x = 2^2 = 4.
    If u=6u=6, then log⁡2x=6  ⟹  x=26=64\log_2 x = 6 \implies x = 2^6 = 64.
    The larger value of xx is 64.

  2. Find the thrust coefficient kk and the final thrust control TT using Model 2.

    Model 2: 32k+1−28(3k)+9=03^{2k+1} - 28(3^k) + 9 = 0
    Rewrite 32k+13^{2k+1} as 32k⋅31=3⋅(3k)23^{2k} \cdot 3^1 = 3 \cdot (3^k)^2:

    3⋅(3k)2−28(3k)+9=03 \cdot (3^k)^2 - 28(3^k) + 9 = 0

    Let v=3kv = 3^k. The equation becomes a quadratic equation in terms of vv:

    3v2−28v+9=03v^2 - 28v + 9 = 0

    Factor the quadratic equation:

    (3v−1)(v−9)=0(3v-1)(v-9) = 0

    This gives two possible values for vv: v=13v=\frac{1}{3} or v=9v=9.
    Substitute back v=3kv = 3^k:
    If v=13v=\frac{1}{3}, then 3k=13  ⟹  3k=3−1  ⟹  k=−13^k = \frac{1}{3} \implies 3^k = 3^{-1} \implies k=-1.
    If v=9v=9, then 3k=9  ⟹  3k=32  ⟹  k=23^k = 9 \implies 3^k = 3^2 \implies k=2.
    The problem states to use the larger value of kk, so k=2k=2.
    Now, calculate the final thrust control TT using T=200kT = 200k:

    T=200⋅2T = 200 \cdot 2 T=400T = 400

    The thrust coefficient kk is 2, and the final thrust control TT is 400.

  3. Find the value of yy using Model 3.

    Model 3: y+5−y−2=1\sqrt{y+5} - \sqrt{y-2} = 1
    Isolate one square root term:

    y+5=1+y−2\sqrt{y+5} = 1 + \sqrt{y-2}

    Square both sides of the equation:

    (y+5)2=(1+y−2)2(\sqrt{y+5})^2 = (1 + \sqrt{y-2})^2 y+5=1+2y−2+(y−2)y+5 = 1 + 2\sqrt{y-2} + (y-2) y+5=y−1+2y−2y+5 = y - 1 + 2\sqrt{y-2}

    Subtract yy from both sides:

    5=−1+2y−25 = -1 + 2\sqrt{y-2}

    Add 1 to both sides:

    6=2y−26 = 2\sqrt{y-2}

    Divide by 2:

    3=y−23 = \sqrt{y-2}

    Square both sides again:

    32=(y−2)23^2 = (\sqrt{y-2})^2 9=y−29 = y-2 y=9+2y = 9+2 y=11y = 11

    Check the solution: 11+5−11−2=16−9=4−3=1\sqrt{11+5} - \sqrt{11-2} = \sqrt{16} - \sqrt{9} = 4 - 3 = 1. The solution is valid.
    The value of yy is 11.

  4. Show that the sum of the results (x+k+y)(x+k+y) satisfies the relationship log⁡2(x+k+y−13)=6\log_2(x+k+y-13) = 6.

    First, calculate the sum x+k+yx+k+y:

    x+k+y=64+2+11=77x+k+y = 64 + 2 + 11 = 77

    Now substitute this sum into the given relationship:

    log⁡2(77−13)=6\log_2(77 - 13) = 6 log⁡2(64)=6\log_2(64) = 6

    Since 26=642^6 = 64, the statement log⁡2(64)=6\log_2(64) = 6 is true.
    Thus, the sum of the results (x+k+y)(x+k+y) satisfies the given relationship.

    The final answers are:

    a) (i) The larger value of the fuel flow rate xx is 64\boxed{64}.

    a) (ii) The thrust coefficient kk is 2\boxed{2} and the final thrust control TT is 400\boxed{400}.

    a) (iii) The value of yy is 11\boxed{11}.

    b) The sum x+k+y=64+2+11=77x+k+y = 64+2+11 = 77. Substituting into the relationship: log⁡2(77−13)=log⁡2(64)=6\log_2(77-13) = \log_2(64) = 6. This shows the relationship is satisfied.

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