AVIA102 Chapter Notes - Chapter 1: Fuselage, Fuel Tank

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redbear503

26 Aug 2016

School

University of Waterloo

Department

Aviation

Course

AVIA102

Professor

Su Yin Tan

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Document Summary

The canard is design that incorporates a horizontal stabilizer at the front of the airplane rather than at the tail. (no tail) o. G a s o l i n e powered, air cooled, internal combustion engine that drives a propeller. Cowling encloses the engine and streamlines the front of the airplane to reduce drag. Cools the engine by ducting cooling air around the engine. Engine mountings are structures made by welding steel tubes together that supports the engine. Firewall is a heavy sheet between the main structure and the engine, with small openings for control lines and fuel. Fuel tank must be behind the firewall and the oil tank must be ahead of it. Fuel tanks can be carried in the wings or in the fuselage: undercarriage (landing gear) The purpose of landing gear is to take the shock of landing and also to support the weight of the airplane and allowing it to maneuver on the ground.

Related Questions

Trolls in halpain land have a gene that determines whether ornot they will have a tail. only trolls that are homozygousrecessive for this gene (alleles T and t) will grow a tail. anothergene (alleles S and s) determines whether this tail will be short,medium, or long because there are three possible phenotypes, youdetermine that this gene displays incomplete dominance. providedthat the extra tail is grown the SS genotype gives a short tail andthe ss genotypes gives a long tail. one day you see two trollsmating. The female troll has a medium lenght tail and the maletroll does not have a tail. The male troll randomly mumbles to youthat he has a genotype of Tt for the epistatic gene and that if hehad a tail, it would be long.

a) what is the probability that a troll offspring has a mediumlenght tail?

b) The trolls have 999 ofspring that curiously all have longtails. What is the probablity that the 1000th troll offspring hastail at all?

c) what is the probability that in the next two of the trolloffspring, one has a long tail and one has no tail?

Please show all work so i can understand the problem

byzantiumwildebeest381

A large marine propulsion diesel engine operating at full load (19810 kW) consumes 184,200 kg/h of air and 3447 kg/h of fuel. The ultimate analysis of the fuel is C 85.7%, H 10.5%, S 2.5%, O 0.4%, N 0.5% (by mass). Use Mair = 28.8 kg/kmol. (a) Write a balanced chemical equation for the reaction assuming complete combustion. (b) Calculate the, % excess air, equivalence ratio, and volumetric analysis of the products

blacksnail806

You are a space explorer of an advanced (therefore alien) civilization. You travel through space with a novel propulsion system based on a perfect (reversible) heat engine. Your ship possesses an infinite heat sink (low temp reservoir) at a temperature of 6.6894 K. You propel your ship by capturing hot asteroids, sucking heat out of them, converting this heat to propulsion work, and expelling the asteriod. How much work (in J) can you obtain from the capture of an asteroid with a temperature of 87.950 K and a heat capacity of 74.259 J/K? (Hint: As the asteroid cools, the efficiency of the engine decreases.) Give your answer to at least four significant figures and do not use scientific notation Answer: Try to relate the differential work to the change in temperature of the asterioid and integrate over the temperature limits I know the correct answer is -4754.59 J, I just have no idea how that answer came about.

AVIA102 Chapter Notes - Chapter 1: Fuselage, Fuel Tank

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