By John Bartlett
From its first visual appeal in 1855 to its lately released 16th variation, Bartlett's standard Quotations has set the traditional for books of quotations. Now, for the 1st time, greater than 900 of the main endearing, expressive, and impassioned sayings approximately love--romantic, passionate, matrimonial, familial, patriotic, spiritual--have been rigorously chosen from the greater than 20,000 quotations in Bartlett's.
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Additional resources for Bartlett's Book of Love Quotations
The above equation is for incompressible fluids. • Q = A2V2 = Cc C v A 2 g (h1 − h2 ) = CA 2 g (h1 − h2 ) in which the product of Cc and Cv is defined as the coefficient of discharge of the orifice. K. Vennard. Diagrams reprinted by permission of John Wiley & Sons, Inc. 43 FLUID MECHANICS (continued) Orifice Discharging Freely Into Atmosphere • where the subscripts p and m stand for prototype and model respectively, and FI FP FV FG FE FT Re We Ca Fr l V Q = CA 2 gh in which h is measured from the liquid surface to the centroid of the orifice opening.
Pi = xipi*, where mass of air Air-Fuel Ratio (A/F): A/F = mass of fuel Stoichiometric (theoretical) air-fuel ratio is the air-fuel ratio calculated from the stoichiometric combustion equation. = partial pressure of component i, xi = mol fraction of component i in the liquid, and pi* = vapor pressure of pure component i at the temperature of the mixture. ( A F )actual × 100 ( A F )stoichiometric ENTROPY ds = (1/T) δQrev ( A F )actual − ( A F )stoichiometric × 100 ( A F )stoichiometric Inequality of Clausius ò (1/T ) δQrev ≤ 0 Percent Theoretical Air = Percent Excess Air = pi s2 – s1 = ò12 (1/T) δQrev ò12 (1/T) δQ ≤ s2 – s1 SECOND LAW OF THERMODYNAMICS Thermal Energy Reservoirs Isothermal, Reversible Process ∆s = s2 – s1 = Q/T ∆Sreservoir = Q/Treservoir , where Q is measured with respect to the reservoir.
E. Hudson. I xc yc , etc. = 0 I xy ,etc. = 0 I xc yc , etc. = 0 MECHANICS OF MATERIALS UNIAXIAL STRESS-STRAIN Uniaxial Loading and Deformation σ = P/A, where Stress-Strain Curve for Mild Steel ♦ σ = stress on the cross section, P = loading, and A = cross-sectional area. ε = δ/L, where δ = longitudinal deformation and L = length of member. E=σ ε= δ= P A δL PL AE THERMAL DEFORMATIONS δt = αL (Τ – Τo), where The slope of the linear portion of the curve equals the modulus of elasticity. δt = deformation caused by a change in temperature, Engineering Strain ε = ∆L / L0, where α = temperature coefficient of expansion, L = length of member, ε = ∆L = engineering strain (units per unit), change in length (units) of member, Τ = Τo = final temperature, and initial temperature.
Bartlett's Book of Love Quotations by John Bartlett