1. The Fourier T ransform of the p robability density, P(x) is
+
T (k) = ( e^(ikx)*P(x)

dx
and is called the characteristic function of the r andom variable x. Let F(k) = log (T(k) and show t hat
a) b) c)
F(0) = 0 F(0) = i<x> F (0) = i<( x)^2>
2. Take P
ME707 MICROSCALE HEAT TRANSFER (Fall 2002) The main objective of the course is to provide students with microscopic understanding of heat transfer phenomena. The course covers the concept of energy carriers  phonon, electron and photon and analytical met
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R OCKET PROPULSION H OME ASSIGNMENT 1 ( Chapters 2 and 10)
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figure. The thrust T is the force necessary to prevent horizontal movement of t he engine. Both engines exhaust a
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Graduate Course Outline and Schedule
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Course name: (Chinese) j (English) Jet Propulsion Theory Course No. Course Objectives: Instructor: MuhRong Wang Credits: 3 Semester: Spring, Fa
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1.1. Definition of a Fluid 1.1.1. Gases 1.1.2. Liquids 1.2. Fluid Thermodynamic Properties 1.2.1. Density 1.2.2. Pressure 1.2.3. Temperature 1.2.4.
MAE 4262: ROCKETS AND MISSION ANALYSIS Fall 2010, Tuesday and Thursday 11:0012:15, Room: S110 Course Website: http:/my.fit.edu/~dkirk/4262 Daniel R. Kirk Email: [email protected] Phone: (321) 6747622 Office: Olin Engineering Center 215 Office Hours: Tuesday
MAE 170: Experimental Techniques Fall 2010
Faculty Prof. Farhat Beg 471, EBUII 8588221266 [email protected] Office hours:Thursdays, 12:30 pm Technical Staff Mike Watson 137 EBUII [email protected] Teaching Assistants Rahul Kapadia Chad Loftis Kevin Mandic
4262: Rockets and Mission Analysis Homework #6
Assigned: November 9, 2010 Due: November 23, 2010
Computerbased Problem: Write a computer code to solve for the adiabatic flame temperature and product composition for hydrogenoxygen combustion over a range
4262: Rockets and Mission Analysis Homework #5b
Assigned: October 14, 2010 Due: November 2, 2010
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Assigned: October 14, 2010 Due: October 21, 2010
Read and review the paper entitled: Advanced Rocket Nozzles by Gerald Hagemann, Hans Immich, Thong Van Nguyen and Gennady Dumnov. A 23 page, double spaced su
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Homework #2
STANJAN or NASA CEA Practice Problem: Consider combustion of a methaneair mixture at 10 atm (both fuel and air are at 10 atm). a. Plot mole fractions, i, for the species CO2, CO, H2O, H2, OH, O2, N2, NO vs. tempe
4262: Rockets and Mission Analysis Homework #1
Assigned: August 24, 2010 Due: September 7, 2010
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Kinetic Theory of Reactive Molecular Gases
Raymond Brun
Universit dAixMarseille, France [email protected]
1.0 INTRODUCTION
In high enthalpy gaseous flows associating high velocities and/or high temperatures, physical and chemical processes such as v
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The equation of motion with nondegenerated terms would be u 2u = a cos( t ) + 2 (1) t y y u = u ; y = t = t ; Introduce nondimensional variables (further, a h primes will be omitted for simplicity). Then, the nondimensional equation one will reduce to
Updates and Corrections to the Solutions to Statistical and Thermal Physics by Harvey Gould and Jan Tobochnik Problem 2.51 Correction Equation (2.54b) should be = (2)(8.314)(300) ln 10 = 11486 J 3.38(a) The limits of the integral in Eq. (S3.47)should be 1
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Page xvi Correction We inadvertently omitted Irwin Oppenheim in our acknowledgements of people who read individual chapters. xvii 57 Ventura Rodriquez should be V
Chapter 7
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c 2010 by Harvey Gould and Jan Tobochnik 7 December 2010 We discuss the nature of the chemical potential by considering some simple models and simulations. We then discuss the role of the chemical pote
Chapter 6
ManyParticle Systems
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Chapter 4
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4.1
Intr
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