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Isolating C on the right-hand sides of both equations, we get sin ( π m ⌊ m ⌋ ) sin β ( ⌊ m ⌋ − N − 1 ) = C = sin ( π m ⌈ m ⌉ ) sin β ( ⌈ m ⌉ − N − 1 ).
Similar(59)
Coupled with structural equations, we get the analyzable models for transonic aeroelasticity in state-space.
Solving the above equations, we get (5.25).
Subtracting the two equations, we get (2.22).
Comparing the above equations, we get (70).
Solving the system of equations, we get.
By solving the above equations, we get (3.11).
(25) Combining the above equations, we get the following theorem.
Solving these equations, we get, which shows that (3.2) is true.
end{cases} By the regularization theory of elliptic equations we get (theta^{0}in C^{2}).
Replacing with and in (1.4), respectively, and subtracting the two resulting equations, we get (2.1).
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Justyna Jupowicz-Kozak
CEO of Professional Science Editing for Scientists @ prosciediting.com