Demystifying the Math of the Coronavirus
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Chapter 30: Quantum Physics ( ) ( )( ( )( ) ( )( ( )( )
Chapter 30: Quantum Physics 9. The tungsten filament in a standard light bulb can be considered a blackbody radiator. Use Wien’s Displacement Law (equation 30-1) to find the peak frequency of the radiation from the tungsten filament. −− 10 1 1 1. (a) Solve Eq. 30-1 fTpeak =×⋅(5.88 10 s K ) for the peak frequency: =×⋅(5.88 1010 s−− 1 K 1 )( 2850 K) =× 1.68 1014 Hz 2. (b) Because the peak frequency is that of infrared electromagnetic radiation, the light bulb radiates more energy in the infrared than the visible part of the spectrum. 10. The image shows two oxygen atoms oscillating back and forth, similar to a mass on a spring. The image also shows the evenly spaced energy levels of the oscillation. Use equation 13-11 to calculate the period of oscillation for the two atoms. Calculate the frequency, using equation 13-1, from the inverse of the period. Multiply the period by Planck’s constant to calculate the spacing of the energy levels. m 1. (a) Set the frequency T = 2π k equal to the inverse of the period: 1 1k 1 1215 N/m f = = = =4.792 × 1013 Hz Tm22ππ1.340× 10−26 kg 2. (b) Multiply the frequency by Planck’s constant: E==×⋅ hf (6.63 10−−34 J s)(4.792 × 1013 Hz) =× 3.18 1020 J 19. The light from a flashlight can be considered as the emission of many photons of the same frequency. The power output is equal to the number of photons emitted per second multiplied by the energy of each photon. -
Multidisciplinary Design Project Engineering Dictionary Version 0.0.2
Multidisciplinary Design Project Engineering Dictionary Version 0.0.2 February 15, 2006 . DRAFT Cambridge-MIT Institute Multidisciplinary Design Project This Dictionary/Glossary of Engineering terms has been compiled to compliment the work developed as part of the Multi-disciplinary Design Project (MDP), which is a programme to develop teaching material and kits to aid the running of mechtronics projects in Universities and Schools. The project is being carried out with support from the Cambridge-MIT Institute undergraduate teaching programe. For more information about the project please visit the MDP website at http://www-mdp.eng.cam.ac.uk or contact Dr. Peter Long Prof. Alex Slocum Cambridge University Engineering Department Massachusetts Institute of Technology Trumpington Street, 77 Massachusetts Ave. Cambridge. Cambridge MA 02139-4307 CB2 1PZ. USA e-mail: [email protected] e-mail: [email protected] tel: +44 (0) 1223 332779 tel: +1 617 253 0012 For information about the CMI initiative please see Cambridge-MIT Institute website :- http://www.cambridge-mit.org CMI CMI, University of Cambridge Massachusetts Institute of Technology 10 Miller’s Yard, 77 Massachusetts Ave. Mill Lane, Cambridge MA 02139-4307 Cambridge. CB2 1RQ. USA tel: +44 (0) 1223 327207 tel. +1 617 253 7732 fax: +44 (0) 1223 765891 fax. +1 617 258 8539 . DRAFT 2 CMI-MDP Programme 1 Introduction This dictionary/glossary has not been developed as a definative work but as a useful reference book for engi- neering students to search when looking for the meaning of a word/phrase. It has been compiled from a number of existing glossaries together with a number of local additions. -
Calculus Terminology
AP Calculus BC Calculus Terminology Absolute Convergence Asymptote Continued Sum Absolute Maximum Average Rate of Change Continuous Function Absolute Minimum Average Value of a Function Continuously Differentiable Function Absolutely Convergent Axis of Rotation Converge Acceleration Boundary Value Problem Converge Absolutely Alternating Series Bounded Function Converge Conditionally Alternating Series Remainder Bounded Sequence Convergence Tests Alternating Series Test Bounds of Integration Convergent Sequence Analytic Methods Calculus Convergent Series Annulus Cartesian Form Critical Number Antiderivative of a Function Cavalieri’s Principle Critical Point Approximation by Differentials Center of Mass Formula Critical Value Arc Length of a Curve Centroid Curly d Area below a Curve Chain Rule Curve Area between Curves Comparison Test Curve Sketching Area of an Ellipse Concave Cusp Area of a Parabolic Segment Concave Down Cylindrical Shell Method Area under a Curve Concave Up Decreasing Function Area Using Parametric Equations Conditional Convergence Definite Integral Area Using Polar Coordinates Constant Term Definite Integral Rules Degenerate Divergent Series Function Operations Del Operator e Fundamental Theorem of Calculus Deleted Neighborhood Ellipsoid GLB Derivative End Behavior Global Maximum Derivative of a Power Series Essential Discontinuity Global Minimum Derivative Rules Explicit Differentiation Golden Spiral Difference Quotient Explicit Function Graphic Methods Differentiable Exponential Decay Greatest Lower Bound Differential -
Slides: Exponential Growth and Decay
Exponential Growth Many quantities grow or decay at a rate proportional to their size. I For example a colony of bacteria may double every hour. I If the size of the colony after t hours is given by y(t), then we can express this information in mathematical language in the form of an equation: dy=dt = 2y: A quantity y that grows or decays at a rate proportional to its size fits in an equation of the form dy = ky: dt I This is a special example of a differential equation because it gives a relationship between a function and one or more of its derivatives. I If k < 0, the above equation is called the law of natural decay and if k > 0, the equation is called the law of natural growth. I A solution to a differential equation is a function y which satisfies the equation. Annette Pilkington Exponential Growth dy(t) Solutions to the Differential Equation dt = ky(t) It is not difficult to see that y(t) = ekt is one solution to the differential dy(t) equation dt = ky(t). I as with antiderivatives, the above differential equation has many solutions. I In fact any function of the form y(t) = Cekt is a solution for any constant C. I We will prove later that every solution to the differential equation above has the form y(t) = Cekt . I Setting t = 0, we get The only solutions to the differential equation dy=dt = ky are the exponential functions y(t) = y(0)ekt Annette Pilkington Exponential Growth dy(t) Solutions to the Differential Equation dt = 2y(t) Here is a picture of three solutions to the differential equation dy=dt = 2y, each with a different value y(0). -
The Exponential Constant E
The exponential constant e mc-bus-expconstant-2009-1 Introduction The letter e is used in many mathematical calculations to stand for a particular number known as the exponential constant. This leaflet provides information about this important constant, and the related exponential function. The exponential constant The exponential constant is an important mathematical constant and is given the symbol e. Its value is approximately 2.718. It has been found that this value occurs so frequently when mathematics is used to model physical and economic phenomena that it is convenient to write simply e. It is often necessary to work out powers of this constant, such as e2, e3 and so on. Your scientific calculator will be programmed to do this already. You should check that you can use your calculator to do this. Look for a button marked ex, and check that e2 =7.389, and e3 = 20.086 In both cases we have quoted the answer to three decimal places although your calculator will give a more accurate answer than this. You should also check that you can evaluate negative and fractional powers of e such as e1/2 =1.649 and e−2 =0.135 The exponential function If we write y = ex we can calculate the value of y as we vary x. Values obtained in this way can be placed in a table. For example: x −3 −2 −1 01 2 3 y = ex 0.050 0.135 0.368 1 2.718 7.389 20.086 This is a table of values of the exponential function ex. -
Calculus Formulas and Theorems
Formulas and Theorems for Reference I. Tbigonometric Formulas l. sin2d+c,cis2d:1 sec2d l*cot20:<:sc:20 +.I sin(-d) : -sitt0 t,rs(-//) = t r1sl/ : -tallH 7. sin(A* B) :sitrAcosB*silBcosA 8. : siri A cos B - siu B <:os,;l 9. cos(A+ B) - cos,4cos B - siuA siriB 10. cos(A- B) : cosA cosB + silrA sirrB 11. 2 sirrd t:osd 12. <'os20- coS2(i - siu20 : 2<'os2o - I - 1 - 2sin20 I 13. tan d : <.rft0 (:ost/ I 14. <:ol0 : sirrd tattH 1 15. (:OS I/ 1 16. cscd - ri" 6i /F tl r(. cos[I ^ -el : sitt d \l 18. -01 : COSA 215 216 Formulas and Theorems II. Differentiation Formulas !(r") - trr:"-1 Q,:I' ]tra-fg'+gf' gJ'-,f g' - * (i) ,l' ,I - (tt(.r))9'(.,') ,i;.[tyt.rt) l'' d, \ (sttt rrJ .* ('oqI' .7, tJ, \ . ./ stll lr dr. l('os J { 1a,,,t,:r) - .,' o.t "11'2 1(<,ot.r') - (,.(,2.r' Q:T rl , (sc'c:.r'J: sPl'.r tall 11 ,7, d, - (<:s<t.r,; - (ls(].]'(rot;.r fr("'),t -.'' ,1 - fr(u") o,'ltrc ,l ,, 1 ' tlll ri - (l.t' .f d,^ --: I -iAl'CSllLl'l t!.r' J1 - rz 1(Arcsi' r) : oT Il12 Formulas and Theorems 2I7 III. Integration Formulas 1. ,f "or:artC 2. [\0,-trrlrl *(' .t "r 3. [,' ,t.,: r^x| (' ,I 4. In' a,,: lL , ,' .l 111Q 5. In., a.r: .rhr.r' .r r (' ,l f 6. sirr.r d.r' - ( os.r'-t C ./ 7. /.,,.r' dr : sitr.i'| (' .t 8. tl:r:hr sec,rl+ C or ln Jccrsrl+ C ,f'r^rr f 9. -
Electrical Power and Energy
Electric Circuits Name: Electrical Power and Energy Read from Lessons 2 and 3 of the Current Electricity chapter at The Physics Classroom: http://www.physicsclassroom.com/Class/circuits/u9l2d.html http://www.physicsclassroom.com/Class/circuits/u9l3d.html MOP Connection: Electric Circuits: sublevel 3 Review: 1. The electric potential at a given location in a circuit is the amount of _____________ per ___________ at that location. The location of highest potential within a circuit is at the _______ ( +, - ) terminal of the battery. As charge moves through the external circuit from the ______ ( +, - ) to the ______ ( +, - ) terminal, the charge loses potential energy. As charge moves through the battery, it gains potential energy. The difference in electric potential between any two locations within the circuit is known as the electric potential difference; it is sometimes called the _____________________ and represented by the symbol ______. The rate at which charge moves past any point along the circuit is known as the ___________________ and is expressed with the unit ________________. The diagram at the right depicts an electric circuit in a car. The rear defroster is connected to the 12-Volt car battery. Several points are labeled along the circuit. Use this diagram for questions #2-#6. 2. Charge flowing through this circuit possesses 0 J of potential energy at point ___. 3. The overall effect of this circuit is to convert ____ energy into ____ energy. a. electrical, chemical b. chemical, mechanical c. thermal, electrical d. chemical, thermal 4. The potential energy of the charge at point A is ___ the potential energy at B. -
Asynchronous Exponential Growth of Semigroups of Nonlinear Operators
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by Elsevier - Publisher Connector JOURNAL OF MATHEMATICAL ANALYSIS AND APPLICATIONS 167, 443467 (1992) Asynchronous Exponential Growth of Semigroups of Nonlinear Operators M GYLLENBERG Lulea University of Technology, Department of Applied Mathematics, S-95187, Lulea, Sweden AND G. F. WEBB* Vanderbilt University, Department of Mathematics, Nashville, Tennessee 37235 Submitted by Ky Fan Received August 9, 1990 The property of asynchronous exponential growth is analyzed for the abstract nonlinear differential equation i’(f) = AZ(~) + F(z(t)), t 2 0, z(0) =x E X, where A is the infinitesimal generator of a semigroup of linear operators in the Banach space X and F is a nonlinear operator in X. Asynchronous exponential growth means that the nonlinear semigroup S(t), I B 0 associated with this problem has the property that there exists i, > 0 and a nonlinear operator Q in X such that the range of Q lies in a one-dimensional subspace of X and lim,,, em”‘S(r)x= Qx for all XE X. It is proved that if the linear semigroup generated by A has asynchronous exponential growth and F satisfies \/F(x)11 < f( llxll) ilxll, where f: [w, --t Iw + and 1” (f(rYr) dr < ~0, then the nonlinear semigroup S(t), t >O has asynchronous exponential growth. The method of proof is a linearization about infinity. Examples from structured population dynamics are given to illustrate the results. 0 1992 Academic Press. Inc. INTRODUCTION The concept of asynchronous exponential growth arises from linear models of cell population dynamics. -
6.4 Exponential Growth and Decay
6.4 Exponential Growth and Decay EEssentialssential QQuestionuestion What are some of the characteristics of exponential growth and exponential decay functions? Predicting a Future Event Work with a partner. It is estimated, that in 1782, there were about 100,000 nesting pairs of bald eagles in the United States. By the 1960s, this number had dropped to about 500 nesting pairs. In 1967, the bald eagle was declared an endangered species in the United States. With protection, the nesting pair population began to increase. Finally, in 2007, the bald eagle was removed from the list of endangered and threatened species. Describe the pattern shown in the graph. Is it exponential growth? Assume the MODELING WITH pattern continues. When will the population return to that of the late 1700s? MATHEMATICS Explain your reasoning. To be profi cient in math, Bald Eagle Nesting Pairs in Lower 48 States you need to apply the y mathematics you know to 9789 solve problems arising in 10,000 everyday life. 8000 6846 6000 5094 4000 3399 1875 2000 1188 Number of nesting pairs 0 1978 1982 1986 1990 1994 1998 2002 2006 x Year Describing a Decay Pattern Work with a partner. A forensic pathologist was called to estimate the time of death of a person. At midnight, the body temperature was 80.5°F and the room temperature was a constant 60°F. One hour later, the body temperature was 78.5°F. a. By what percent did the difference between the body temperature and the room temperature drop during the hour? b. Assume that the original body temperature was 98.6°F. -
Control Structures in Programs and Computational Complexity
Control Structures in Programs and Computational Complexity Habilitationsschrift zur Erlangung des akademischen Grades Dr. rer. nat. habil. vorgelegt der Fakultat¨ fur¨ Informatik und Automatisierung an der Technischen Universitat¨ Ilmenau von Dr. rer. nat. Karl–Heinz Niggl 26. November 2001 2 Referees: Prof. Dr. Klaus Ambos-Spies Prof. Dr.(USA) Martin Dietzfelbinger Prof. Dr. Neil Jones Day of Defence: 2nd May 2002 In the present version, misprints are corrected in accordance with the referee’s comments, and some proofs (Theorem 3.5.5 and Lemma 4.5.7) are partly rearranged or streamlined. Abstract This thesis is concerned with analysing the impact of nesting (restricted) control structures in programs, such as primitive recursion or loop statements, on the running time or computational complexity. The method obtained gives insight as to why some nesting of control structures may cause a blow up in computational complexity, while others do not. The method is demonstrated for three types of programming languages. Programs of the first type are given as lambda terms over ground-type variables enriched with constants for primitive recursion or recursion on notation. A second is concerned with ordinary loop pro- grams and stack programs, that is, loop programs with stacks over an arbitrary but fixed alphabet, supporting a suitable loop concept over stacks. Programs of the third type are given as terms in the simply typed lambda calculus enriched with constants for recursion on notation in all finite types. As for the first kind of programs, each program t is uniformly assigned a measure µ(t), being a natural number computable from the syntax of t. -
Best Glide Speed and Distance
General Aviation FAA Joint Steering Committee Aviation Safety Safety Enhancement Topic Best Glide Speed and Distance The General Aviation Joint Steering Committee (GAJSC) has determined that a significant number of general aviation fatalities could be avoided if pilots were better informed and trained in determining and flying their aircraft at the best glide speed while maneuvering to complete a forced landing. What is Best Glide Speed? Keep in mind that this speed will increase with weight so most manufacturers will establish Is it the speed that will get you the greatest the best glide speed at gross weight for the aircraft. distance? Or is it the speed that gets you the That means your best glide speed will be a little longest time in the air? Or are these two the same lower for lower aircraft weights. — the longer you fly, the further you go? Well, as so often is the case, best glide speed depends on what Need More Time? you’re trying to do. If you’re more interested in staying in the air Going the Distance as long as possible to either fix the problem or to communicate your intentions and prepare for a If it’s distance you want, than you’ll need to forced landing, then minimum sink speed is what use the speed and configuration that will get you you’ll need. This speed is rarely found in Pilot the most distance forward for each increment of Operating Handbooks, but it will be a little slower altitude lost. This is often referred to as best glide than maximum glide range speed. -
Inertia and Rate of Change of Frequency (Rocof)
Inertia and Rate of Change of Frequency (RoCoF) Version 17 SPD – Inertia TF 16. Dec. 2020 ENTSO-E AISBL • Rue de Spa 8 • 1000 Brussels • Belgium • Tel + 32 2 741 09 50 • Fax + 32 2 741 09 51 • [email protected] • www. entsoe.eu Inertia and Rate of Change of Frequency (RoCoF) 1. Executive Summary ............................................................................................................... 3 2. Introduction and Aim of the Document ................................................................................... 4 3. Definitions .............................................................................................................................. 6 3.1 Inertia ................................................................................................................................. 6 3.2 Rate of Change of Frequency (RoCoF) .............................................................................. 8 3.3 Centre of Inertia .................................................................................................................. 9 4. Impact of Inertia on Power Systems ..................................................................................... 11 4.1 Frequency and Voltage Control of Generators .................................................................. 11 4.2 Stability ................................................................................................................................. 12 4.3 Protection Equipment ......................................................................................................