[T] An airplane’s Mach number M is the ratio of its speed to the speed of sound. When a plane is flying at a constant altitude, then its Mach angle is given by μ = 2 sin − 1 ( 1 M ) . Find the Mach angle (to the nearest degree) for the following numbers. a . μ = 1.4 b . μ = 2.8 c . μ = 4.3
[T] An airplane’s Mach number M is the ratio of its speed to the speed of sound. When a plane is flying at a constant altitude, then its Mach angle is given by μ = 2 sin − 1 ( 1 M ) . Find the Mach angle (to the nearest degree) for the following numbers. a . μ = 1.4 b . μ = 2.8 c . μ = 4.3
[T] An airplane’s Mach number M is the ratio of its speed to the speed of sound. When a plane is flying at a constant altitude, then its Mach angle is given by
μ
=
2
sin
−
1
(
1
M
)
. Find the Mach angle (to the nearest degree) for the following numbers.
a) Find the scalars p, q, r, s, k1, and k2.
b) Is there a different linearly independent eigenvector associated to either k1 or k2? If yes,find it. If no, briefly explain.
Plz no chatgpt answer Plz
Will upvote
1/ Solve the following:
1 x +
X + cos(3X)
-75
-1
2
2
(5+1) e
5² + 5 + 1
3 L
-1
1
5² (5²+1)
1
5(5-5)
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