Engineering, 21.08.2019 21:30 aryal191
Aprojectile in flight canties with it a more or less conical-shaped shock front. from physical reasoning it appears that at great distance from the projectile this shock wave becomes truly conical and changes in vclocity and density across the shock becomes vanishingly small. photographs of a bullet in light show that at a great distance from the bullet the lotal included angle of the conç is 50,30°. the pressure and lymperature of the undisturbed air ir 100.801 kpa and 22.78°c. respectively. calculate thç velocity of the bullet, and the mach number of the bullcl. relative lu the undisturbed air.
Answers: 1
Engineering, 04.07.2019 18:10
Draw the engineering stress-strain curve for (a) bcc; (b) fcc metals and mark important points.
Answers: 1
Engineering, 04.07.2019 18:10
Hydraulic fluid with a sg. of 0.78 is flowing through a 1.5 in. i.d. pipe at 58 gal/min. the fluid has an absolute viscosity of 11.8 x 105 lbf-sec/ft2. is the flow laminar, turbulent or within the critical range? give both a numerical reynolds number and a term answer.
Answers: 3
Engineering, 04.07.2019 18:20
Find the minimum film thickness for a journal bearing with the data below. shaft diameter, d-50 mm, clearance ratio, cdratio? 0.001, shaft speed, n 2000 rpm; bearing length. i 200 mm; eccentricity ration, ? -0.55. ( note, cdratio-ca/d) the minimum film thickness is um
Answers: 2
Engineering, 04.07.2019 18:20
Air flows over a heated plate àt a velocity of 50m/s. the local skin factor coefficient at a point on a plate is 0.004. estimate the local heat transfer coefficient at this point.the following property data for air are given: density = 0.88kg/m3 , viscosity 2.286 x 10 ^-5 kgm/s , k = 0.035w/mk ,cp = 1.001kj/kgk. use colburn reynolds analogy.
Answers: 1
Aprojectile in flight canties with it a more or less conical-shaped shock front. from physical reaso...
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