The altitude h [ft] attained by an aircraft climbing from sea level at its maximum rate of climb [ft/min] is shown at four times t [min]. index, i: 1 2 3 4 ti [min]: h; [ft]: ! 10 20 30 40 5400 9000 11600 12800 Estimate the aircraft's rate of climb (dh/dt)3 when it is at an altitude of 11600 ft by the following techniques.
The altitude h [ft] attained by an aircraft climbing from sea level at its maximum rate of climb [ft/min] is shown at four times t [min]. index, i: 1 2 3 4 ti [min]: h; [ft]: ! 10 20 30 40 5400 9000 11600 12800 Estimate the aircraft's rate of climb (dh/dt)3 when it is at an altitude of 11600 ft by the following techniques.
Chapter6: Exponential And Logarithmic Functions
Section6.1: Exponential Functions
Problem 60SE: The formula for the amount A in an investmentaccount with a nominal interest rate r at any timet is...
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