Search Results for weights

Fig. 15 Relative weights of different structural configurations More

Fig. 42 Impeller shoes in ASTM A52 class III type A. Weights are 5, 13, and 22 kg (11, 28, and 49 lb). Courtesy of Wear-Tek, Inc. More

Fig. 30 Relative weights of aluminum and carbon/epoxy composite structures. Failure strains are less for loaded holes, for using statistical basis rather than average, and for larger holes. Reliance on benefit from interference-fit fasteners requires absolutely no net or loose-fit bolts More

Fig. 3 Solute distribution curve (weight percent copper vs. weight fraction solid contained) for three cases of Al-4.5%Cu alloy: equilibrium (Eq: α → ∞), Gulliver-Scheil (G-S; α → 0), and directional solidification with α = 0.5. For equilibrium, the final as-cast solute distribution (Eq-final More

Fig. 11 Actual and percent weight gain and percent weight reduction by coating with time of IMI 834 alloy (Ti-5.8%Al-4%Sn-3.5%Zr-0.7%Nb-0.5%Mo-0.3%Si) at 800 °C (1472 °F) up to 400 h. Adapted from Ref 10 , 17 More

Fig. 17 Overall temperature-time, weight-time, and weight-temperature curves for conventional binder burnout and sintering of ceramic multilayer capacitors More

Fig. 17 Coating weight loss as a function of number of revolutions. (a) Weight loss values after 10,000 revolutions as a function of coating thickness. (b) Point represented by red circle indicates the coating annealed at 373 K (100 °C, or 212 °F). Source: Ref 57 More

Fig. 41 Mating drop-weight tear test fractures in ship steel showing the influence of test temperature of fracture appearance. Note that chevrons are most clearly developed at −45 °C (−50 °F). The fractures were located by the notch at the top of each specimen. More

Fig. 8 Thermogravimetric analysis thermogram showing the weight-loss profile for a typical plastic resin More

Fig. 37 Thermogravimetric analysis weight-loss profile comparison showing a reduction in the thermal stability of the discolored surface material relative to the base material More

Fig. 2 Increased use of refractory metals in nickel-base superalloys. (a) Weight percent. (b) Atomic percent More

Fig. 39 Components of a weight coat system including (1) corrosion-protective coating and (2) reinforced concrete outer layer More

Fig. 7 Typical effects of weight and quantity on the cost of magnesium die castings. On a weight basis, the cost of die castings heavier than about 0.15 kg ( 1 3 lb) is fairly constant. For lighter castings, those weighing less than about 0.10 for 0.15 kg (4 or 5 oz), the cost per More

Fig. 37 Preformed aircraft skin section chemically contoured to reduce weight. Dimensions given in inches More

Fig. 3 Relative weight loss versus billet temperature as a function of heating environment and method of cooling. WQ, water quench. Source: Ref 2 More

Fig. 22 Damage diameter versus impacter kinetic energy for falling-weight impact tests and gas-gun tests conducted on [45/0/−45/90] 6s AS4/3501-6 laminates More

Fig. 16 Example of cost and weight savings obtainable using superplastic forming in the aircraft industry. Conventionally fabricated part (a) had 15 pieces and required 212 fasteners; the superplastically formed part (b) consists of 3 parts and requires 45 fasteners. This results in a 56% cost More

Fig. 21 Comparison of different methods of weighting the results of measurements: number- and area-weighted distributions of grain section areas More

Fig. 25 Corrosion weight loss and corrosion rate of various 316 stainless steels in 10% HCl water solution. Source: Ref 22 More

Fig. 8 Relation of the volume of oil and weight of work quenched in relation to the temperature rise of the oil More