what is the net work output of paths ABCDA and ABDA
since the work done for a cyclic process is given by enclosed area on pv diagram..
so first calculate work done for path ABCDA:
work done for path ABCDA is area enclosed by ABCDA;
area ABCDA= area of triangle ABD+area of triangle CDB;
area of ABD=0.5*(2.6-1)*(4-1)=2.4;
area of CDB=(0.5)*(2-0.6)*(4-1)=2.1;
so area enclosed by ABCDA =4.5 =work done in ABCDA ;
so area for the path ABCDA =4.5 J.
work done for path ABDA = area of traingle ABD;
as calculated above area of triangle ABD =2.4;
so work done in process ABDA =2.4 J.
hence work done for path ABCDA =4.5J,
work done for path ABDA =2.4J.
what is the net work output of paths ABCDA and ABDA p (106 N/m2) А 2.6...
Calculate the net work output (in J) of a heat engine following path ABCDA in the figure, where V1 = 3.0 ✕ 10−3 m3 and V2 = 12.0 ✕ 10−3 m3.
Rating answers ! Please show your work! THank you (25%) Problem 2: Consider a heat engine with a cycle described by the figure, with the (10 N/m2) volume and pressure at points A. B. C, and D given below Randomized Variables VA 1.15 x 10-3 m3 PA 2.5 x 106 N/m2 PB 2.12 x 106 N/m2 PC = 0.45 × 106 N/m2 P 0.93 x 106 N/m2 Va V (10-*m) Otheexpertta.com Calculate the net work output, in joules, of the...
determine 1) the maximum stress in the bar if P=9kN. 3.0 3.2 2.8 WW 2.6 3.0 N W 2.4 N hi 2.8 2.2 svg (w - 21) K - 4.0 K 2.0 2.6 3.01 2.0 1.8 w IS 2.4 1.6 w h 1.2- 1.1 1.4 2.2 LATIN . 1.2 2.0 1.0 0 0.1 0.6 0.7 0.8 0.9 1.0 0.5 0.2 0.3 2r 0 0.4 0.5 0.1 0.2 0.3 0.4 h 3.2 mm 48 mm 32 mm Р P r =...
(6%) Problem 7: A certain heat engine performs a cycle described by the curve A-BCDA in the p-V diagram shown in the figure. The segments between the designated points are all straight. The values of the pressures and volumes at the designated points are: Р(10° Ра) А РА Рв Randomized Variables VA 0.65 x 10-3 m' В VB 3.7 x 10-3 m3 D PA = 2.65 x 106 N/m2 РD Рс PB 1.92 x 106 N/m2 Pc 0.65 x 106...
0.06 moles of a monatomic gas undergoes the cycle A ⟶B⟶C⟶A as shown on the P-V diagram below. In the transition A⟶B the gas expands adiabatically and the temperature drops from 600K to 400K. What is △U for this transition? What is the work done on the gas? (This is the answer to (a) in the table below) During the transition B⟶C, the volume decreases from 2x10-3 m3 to 1x10-3 m3 at constant atmospheric pressure (isobaric). What is the work...
0.06 moles of a monatomic gas undergoes the cycle A ⟶B⟶C⟶A as shown on the P-V diagram below. In the transition A⟶B the gas expands adiabatically and the temperature drops from 600K to 400K. What is △U for this transition? What is the work done on the gas? (This is the answer to (a) in the table below) During the transition B⟶C, the volume decreases from 2x10-3 m3 to 1x10-3 m3 at constant atmospheric pressure (isobaric). What is the work...
An object of mass 0.50 kg weighs 2.0 N when it is 1.0 × 106 m above the surface of Planet X. The radius of the planet is 4.0 × 106 m. What free-fall acceleration will the 0.50-kg object experience when at the surface of Planet X? A) 2.0 m/s2 B) 6.3 m/s2 C) 4.0 m/s2 D) 4.8 m/s2
The pressure increases by 1.0 x 104 N/m2 for every meter of depth beneath the surface of the ocean. At what depth does the volume of a Pyrex (bulk modulus 2.6 x 1010 N/m2) glass cube, 1.2 x 10-2 m on an edge at the ocean's surface, decrease by 9.3 x 10-10 m3
TB4 The PV diagram in the figure is for n moles of an ideal monatomic gas. The gas is initially at point A. The paths AD and BC represent isothermal changes. R is the universal gas constant. Let the pressures, volumes, and temperatures at the labeled points be denoted as PA , PB, etc., and VA , VB, etc., and TA, TB, etc., respectively. If the system is brought to point C along th<e path A-»E->C, what is the heat...
this answer it say wrong!! 3767374.8 N = 3.76 x 106 N What is the net upward force (in N) on an airplane wing of area A-21.0 m2 if air streams at 2.96 × 102 m/s across its top and at 2.69 × 102 m/s past the bottom? Note that this airplane moves at subsonic speed, which is less than the speed of sound (called Mach 1, about 3.3 × 102 m/s). (Assume the density of air is 1.2 kg/m3....