How about some problems that are actually trickier to solve:
1. A stick of length one is split into two sticks at a random point that is uniformly distributed -- say X is the shorter stick and Y is the longer one. Find E(X) and Var(X), then find E(Y-X)^2
2. Leonid and Rubix are alternating rolling a pair of dice, stopping either when Leonid rolls the sum of 9 or when Rubix rolls the sum of 6. Assuming that Leonid rolls first, find the probability that Leonid has the final roll.
3. Easier one for ya -- you can buy a lottery ticket for $1. If you win, you get $5 back. You're determined to win twice at any cost. Each ticket has p = .125 of winning. What is the probability you get your second winning ticket on the sixth purchase? What's your expected profit or loss from this lottery in general?
Originally posted by MrRubix
Here's a hard one I doubt anyone here will get -- from one of my homeworks:
You have a system of N components. Each component will function, independently, with probability p. The total system of components will work if at least half of them are functioning. For what value of p is a 5-component system more likely to operate than a 3-component system? How about a (2k+1) component system over a (2k-1) component system?
Statistics is a world I'm glad I never had to enter.
What is the specific thrust of a turbojet engine with compressor pressure ratio 20, design Mach number 1.6, turbine inlet temp 1400K flying at 35,000 ft? Turbine and Compressor polytropic efficiency .95, isentropic effenciency .97, Gamma 1.4.
Here's a hard one I doubt anyone here will get -- from one of my homeworks:
You have a system of N components. Each component will function, independently, with probability p. The total system of components will work if at least half of them are functioning. For what value of p is a 5-component system more likely to operate than a 3-component system? How about a (2k+1) component system over a (2k-1) component system?
do we win credits if we get the correct answer? lol
1st in Kommisar's 2009 SM Tournament 1st in I Love You`s 2009 New Year`s Tournament 3rd in EnR's Mashfest '08 tournament 5th in Phynx's Unofficial FFR Tournament 9th in D3 of the 2008-2009 4th Official FFR Tournament 10th in D5 of the 2010 5th Official FFR Tournament 10th in D6 of the 2011-2012 6th Official FFR Tournament FMO AAA Count:71 FGO AAA Count:10
I've gotta go for now but I'll give JKPolk's question a shot later -- looks like it's just a matter of throwing together some aerospace equations, but I only have a basic idea of how those variables would relate (and no idea where the gamma fits in). Also wtf is isosdmkflmdsklmfsdklopic efficiency.
Statistics is a world I'm glad I never had to enter.
I took my one quarter of mandated statistics for engineers and peaced the **** out. Not looking at that **** again.
Originally posted by JKPolk
What is the specific thrust of a turbojet engine with compressor pressure ratio 20, design Mach number 1.6, turbine inlet temp 1400K flying at 35,000 ft? Turbine and Compressor polytropic efficiency .95, isentropic effenciency .97, Gamma 1.4.
You're speaking my language, man!
@Rubix, Gamma is just the ratio of specific heat to specific volume, a common property for air. Rocket exhausts with fuel mixed into them are usually a gamma of 1.3.
EDIT: in an ideal situation, isentropic efficiency is 100%, meaning that it's entirely adiabatic and the process is reversible. Since we know that turbojets don't function at an ideal capacity in a real situation, the .97 is to make up for things like heat loss through the walls of the turbojet, etc.
Given Variables
N[H]=1
N[L]=5
P[H][q]=40-q
P[L][q]=20-2q
MC=1
Area of a trapezium: .5(a+b)c
S[H][q]= ((40+40-q)q/2 = 40q -.5q^2 for all q<=40, 800 for all q>40
S[L][q]= ((20+20-2q)q/2 = 20q - q^2 for all q<=10, 100 for all q>10
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