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An aircraft with wing aft tail configuration has tail efficiency of 0.95 and tail volume ratio of horizontal tail is 0.7. Determine pitching moment coefficient slope for the tail. Given lift curve slope of tail is 4.2 per rad. Consider downwash derivative as 0.6.
A typical jet transport aircraft needs to be sized based on following parameters. Wing area S=50m2, MAC=5m. If tail volume coefficient of horizontal tail is 1 and tail area is 10m2 then, find the required tail moment arm.
The figure shows the plot of y as a function of x
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The function shown is the solution of the differential equation (assuming all initial conditions to be zero) is
A language with string manipulation facilities uses the following operations. head(s) - returns the first character of the strings tail(s) - returns all but the first character of the strings concat (s1, s2) - concatenates string s1 with s2. The output of concat (head(s), head(tail(tail(s)))), where s is acbc is
Consider the following statements: 1. A differential amplifier is used at the input stage of an operational amplifier 2. Differential amplifiers have very high CMRR Which of these statements are correct?
Introducing FET differential amplifier pair at the input stage of differential amplifier produces
When the input of differential amplifier V1 = 0, then the differential amplifier is said to be operated in
The Common Mode Rejection Ratio (CMRR) of a differential amplifier using an operational amplifier is 100 dB. The output voltage for a differential input of 200 μV is 2 V. The common mode gain is
The tail current in a differential amplifier equals .
Define total current (IQ) equation in differential amplifier with constant current bias current