Dynamics cheat sheet

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$my Latex and Tex4ht cheat sheet$

Image from http://edition.cnn.com/2014/01/16/travel/inside-airbus-beluga/index.html?hpt=ibu_ c2 Image from http://www.nasa.gov/centers/dryden/Features/super_guppy.html 118
Image from http://www.aerospaceweb.org/question/aerodynamics/q0130.shtml ”Boeing Pelican ground effect vehicle” 19.6 links 1. https://3dwarehouse.sketchup.com/search.html?redirect=1&tags=airplane 19.7 references 1. Etkin and Reid, <strong>Dynamics</strong> of flight, 3rd edition. 2. Cook, Flight <strong>Dynamics</strong> principles, third edition. 3. Lecture notes, EMA 523 flight dynamics and control, University of Wisconsin, Madison by Professor Riccardo Bonazza 4. Kuethe and Chow, Foundations of Aerodynamics, 4th edition 119
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Dynamics cheat sheet Nasser M. Abba
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18.7.2 Bi-Elliptic transfer orbit .
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are the natural frequencies of the
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Similarly, µ 2 is found ⎧ ⎫T
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Or in full form and ⎧ ⎫ ⎡ ⎨
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Hence The first eigen vector is Sim
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The transformation from modal coord
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Where F n = 2 T F 0 = 2 T ∫ T 0
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Let z = Re { Ze iωt} , z ′ = Re
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Now, u = Re { Ue iωt} , u ′ = Re
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Hence at t = 0 the phase of the res
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The following table gives the solut
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5.3 no loading (free) mu ′′ + c
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5.5 Impulse sin function Input is g
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Solution to single degree of freedo
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7 Some common formulas These defini
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8 Derivation of the solutions of th
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8.2.2 under-damped ζ < 1 The gener
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When ϖ ≈ ω but less than ω, le
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Hence the full solution is u p = p
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8.4 Response to impulsive loading 8
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where A = B = F 0 m 2ω √ ξ 2
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where ∆ is very small positive qu
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at t = t 1 ˙u (t 1 ) = −ξωe
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8.5 references 1. Vibration analysi
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11 Formulas sin 2 x 1cos2x 2 cos 2
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12 Velocity and acceleration diagra
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12.3 spring pendulum with block mov
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13 Velocity and acceleration of rig
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14.2 3D Not Using vehicle dynamics
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14.2.2 Derivation for τ = Iω in 3
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15 Wheel spinning precession x Mg
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18 Astrodynamics 18.1 Ellipse main
Page 67 and 68: magnitude of ⃗r period T mean sat
Page 69 and 70: 18.3 Flight path angle for ellipse
Page 71 and 72: This diagram below from Orbital mec
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Page 75 and 76: 18.7.3 semi-tangential elliptical t
Page 77 and 78: 18.8.1 Rocket equation with plane c
Page 79 and 80: 18.10 interplanetary transfer orbit
Page 81 and 82: 2. Find speed of second planet V 2
Page 83 and 84: 1 mu = 324859; 2 alt = 1475.776; 3
Page 85 and 86: 18.11.3 Two satellite, separate orb
Page 87 and 88: 1 TOF:=hohmann_rendezvous_2(theta=0
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Page 91 and 92: 18.14 Orbit changing by low contiuo
Page 93 and 94: C r below is the core chord of the
Page 95 and 96: 1 C L = ∂C L ∂α α = C Lα α
Page 97 and 98: 1 2 3 C Lwb = ∂C L wb ∂α wb α
Page 99 and 100: 2. stall from http://en.wikipedia.o
Page 101 and 102: http://en.wikipedia.org/wiki/Flight
Page 103 and 104: http://www.grc.nasa.gov/WWW/k-12/UE
Page 105 and 106: http://en.wikipedia.org/wiki/Lift_c
Page 107 and 108: http://adamone.rchomepage.com/cg_ca
Page 109 and 110: From http://www.solar-city.net/2010
Page 111 and 112: Page 184, flight dynamics principle
Page 113 and 114: Image from http://www.americanflyer
Page 115 and 116: From FAA pilot’s handbook I do no
Page 117: zero-lift angle The angle of attack
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Dynamics cheat sheet

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