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Maximum speed -Pro craft
The standard approach for prop-driven aircraft is to assume that engine and propeller together produce a power (as opposed to thrust) output that is independent of speed. Calculations analogous to those carried out above for the jet aircraft, but based on power rather than drag, lead to formulae for maximum speed, absolute ceiling, and so on. The resulting equations do not however lend themselves to simple closed-form solutions, and generally, iterative solutions need to be found. Suppose the maximum engine shaft power output is Pmax. The propeller will convert this to useful propulsive power with an efficiency η ; the useful available propulsive power is thus given by Pav = η Pmax
2 horizontal flate plate 0.15mm apart and space between them is filled with an oil having viscosity 1poise the upper plate of area 1.5m2 is required to move with a speed of 0.5m/se
Equivalent Shaft Horsepower (EHP) In practice there is always a certain amount of jet thrust in the total output of the turbo-propeller engine and this must be added to the s.h
Measurements of Economic Worth There are several methods of economic worth used to compare alternatives. If you decide to use present worth analysis, then you have indicate a
Q. Describe briefly the following methods of forging : (i) Drop forging (ii) press forging Ans. (i) Drop Forging: It is also called die
limitations of nernsts law
Convert the analog filter the system function Ha(s)=(s+0.1)/((s+0.1)(s+0.1)+16) with digital iir filter by bilinear transformation .the digital filter is to have the resonent freq
Describe the principle parts of a quality function deployment matrix
Go to https://blackboard.newhaven.edu/ user: user:Aaldo6 Pass:1992May239645 Class: fire 2209 Occup safety$ hilt-fire take the test its one hour test multiple choices its due t
what is function independence.on software engineering
answer
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