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Flight dynmaics
The study of aircraft- Stability & Trim (Equilibrium)- Motion due to
• Control inputs
• Atmospheric Disturbances
• We will consider for the most part fixed-wing aircraft
• Subject builds on
- Mechanics (Statics & Dynamics)
- Aerodynamics
- Contro
ENGINE CYCLES The two commonly used cycles on which the I.C. engines operate are: 1Otto cycle. 2 Diesel cycle. 1 OTTO CYCLE: theoretical Otto cycle is shown i
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Depreciation Calculation Two most popular methods of charging depreciation are: straight line and diminishing balance or written-down value (WDV) methods. For reporting to the sha
Spectrum of Data Pulses As the waveform period increases, the fundamental frequency of the spectrum decreases and the harmonics become more closely spaced. In the limit, as
1- plot and creat x1(t)=4exp(t/5),x2(t)=Sin(2pift+Pi/2) 2-write a c fucntion to compute convolution of n2 finite series ands plot 3-implemet an FIR filter in c in CCS
A heat recovery device involves transferring energy from hot flue gases passing counter currently through an annular region to pressurized water flowing through the inner tube of t
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A steel cylinder 10 cm in diameter and 10 cm long is initially at 300 0C. it is immersed in an oil bath which is maintained at 40 0C, with h= 280 W/m2. 0C. Find the temperature at
Aerospace propulsion is essentially based on Newton'slaws of motion (1687): • A body on which there is no resultant force will move ina straight line with constant velocity.
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