Applied Computational Fluid Dynamics Techniques - Wiley Episode 1 Part 5 ppsx

... 211 11 .8Projectivepredictionofpressureincrements 212 11 .9Examples 213 11 .9 .1 vonKarmanvortexstreet 213 11 .9.2 NACA0 012 wing . 216 11 .9.3 LPD -1 7 topsideflowstudy 218 11 .9.4 DARPASUBOFFmodel 223 11 .9 .5 ... the items 28 APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES 2 31 4 5 6 1 3 54 6 2 2 3 1 4 5 6 2 34 5 6 1 2 34 5 6 1 1 3 5 6 2 4 6 25 4 3...

Ngày tải lên: 27/06/2014, 08:20

... ICL > ;10 3 3-D FEFLO30 19 85 Forebody Cyber-2 05 > ;10 4 2-D FEFLO27 19 86 Train Cray-XMP > ;10 5 3-D FEFLO72 19 89 Train Cray-2 > ;10 6 3-D FEFLO74 19 91 T-62 Tank Cray-2 > ;10 7 3-D FEFLO96 19 94 ... Split Unregistered Version - http://www.simpopdf.com 8 APPLIED COMPUTATIONAL FLUID DYNAMICS TECHNIQUES 12 3 4 5 6 7 8 910 11 12 13 1 2 3 4 5 6 7...

Ngày tải lên: 27/06/2014, 14:20

... shown in Figure 5 .12 FIGURE 5 .10 : DeVlieg tooling for single- or multi-spindle automatic lathe (Courtesy: National Acme Co., Div. DeVlieg-Bullard Inc.) FIGURE 5 .11 : Conventional single-spindle automatic ... Inc.) FIGURE 5 .13 : Multiple-spindle vertical automatic chucking machine. (Courtesy National Acme Co., Div. DeVlieg-Bullard Inc.) FIGURE 5 .14 : Multi-station tool holder...

Ngày tải lên: 21/07/2014, 15:20

... at 10 .000mm +0 .50 0 /-0 .000. 1 10.042 11 10 .022 2 10 .029 12 10 .030 3 10 .0 31 13 10 . 012 4 10 .029 14 10 .048 5 10 . 011 15 10 .099 6 10 . 054 16 10 . 0 15 7 10 .0 25 17 10 .023 8 10 .0 31 18 10 .034 9 10 .047 19 10 .042 10 10 . 016 20 10 . 053 •What ... understand 10 9 19 1 Easy to carry/handle 6 7 13 5 Good aesthetics 4 8 12 5 Cont...

Ngày tải lên: 21/07/2014, 17:20

... 1 0-3 0 20 0.0 25 2 3 0-7 0 50 0.027 3 7 0-9 0 80 0.039 4 9 0 -1 50 12 0 0.066 5 15 0 -1 90 17 0 0.0 95 6 19 0-2 10 200 0 .11 5 7 21 0-2 90 250 0 .12 6 8 29 0-4 10 350 0 .12 4 9 41 0-4 90 450 0 .11 3 10 49 0-6 10 55 0 ... 60 1. 5 27 .5 27 .5 8.5e-04 50 1. 7 27 .5 27 .5 8.6e-04 25 1. 83 26 26 8.7e-04 15 2 .52 25. 4 25. 4 8.8e-04 CF...

Ngày tải lên: 28/06/2014, 16:20

... from x = 16 5 to x = 16 6. III. For x = 16 5, the denominator is 16 5 2 – 16 5 = (16 5) (16 5 – 1) = (16 5) (16 4), and for x = 16 6, the denominator is 16 6 2 – 16 6 = (16 6) (16 6 – 1) = (16 6) (16 5) .  erefore, ... can be solved for n: 55 50 90 1 = + + n n 55 (n + 1) = 50 n + 90 multiply both sides by (n + 1) 55 n + 55 = 50 n + 90 distribute...

Ngày tải lên: 22/07/2014, 14:20

... between (A) 290 12 .5 and 290 11 .5 (B) 2 95 12 and 2 85 11 .5 (C) 2 85 12 and 2 95 12 (D) 2 85 12 .5 and 2 95 11 .5 (E) 2 95 12 .5 and 2 85 11 .5 x 12 34 1 2–4 5 –3 5 0 13 0. Which of the following ... as a vverage= + = + = + == 812 3 8 4 15 1 4 12 8 99 8 4 61 4 12 99 61 12 16 0 12 13 11 3 .  e correct answer is A. 15 . 0 .1...

Ngày tải lên: 22/07/2014, 14:20

... ∅ .5 01 + ∅.0 05 = ∅ .50 6. The hole has an MMC size limit of ∅. 51 1 and a positional tolerance of ∅.0 05 at MMC. Since it’s an internal feature of size, its virtual condition is ∅. 51 1 − ∅.0 05 = ∅ .50 6. ... Tolerancing 5- 5 3 LMC, it establishes a Level 2 virtual condition boundary as described in section 5. 6.3 .1 and Figs. 5 -1 7(b) and 5 -1 8(b). Alternatively, the “center...

Ngày tải lên: 21/07/2014, 15:20

... section 5. 8 .5. Figure 5 -1 5 Conformance to limits of size for a width-type feature Figure 5 -1 6 Size limit boundaries control circularity at each cross section 5- 2 4 Chapter Five 5. 6.2 .1 Modifier ... Rule #1 mandates a ∅ .50 2 boundary of perfect form at MMC (envelope) Figure 5- 2 1 Rule #1 specifies a boundary of perfect form at MMC Geometric Dimensioning and Toleranc...

Ngày tải lên: 21/07/2014, 15:20

... designer’s expectations. Fig. 3-2 e shows a combination of Figs. 3-2 b and 3-2 c (like Figs. 3 -1 b and 3 -1 c), in that it allows the shape to be small at one end and large at the other. Unlike Figs. 3 -1 b and 3 -1 c, Fig. 3-2 e ... subcommittees, including Y14 Main Committee, Y14.3 Multiview and Sectional View Drawings, Y14 .5 Dimensioning and Tolerancing, Y14 .11 Molded Par...

Ngày tải lên: 21/07/2014, 15:20