SEM-2016(03)-II MECHANICAL ENGINEERING. Paper -11. Please read each of the following instructions carefully before. attempting questions.

Similar documents
SEM-2017(03HI MECHANICAL ENGINEERING. Paper II. Please read each of the following instructions carefully before attempting questions.

MECHANICAL ENGINEERING

S.E. (Chemical) (Second Semester) EXAMINATION, 2011 HEAT TRANSFER (2008 PATTERN) Time : Three Hours Maximum Marks : 100

BME-A PREVIOUS YEAR QUESTIONS

UNIT I Basic concepts and Work & Heat Transfer

R13 SET - 1 '' ''' '' ' '''' Code No RT21033

MAHALAKSHMI ENGINEERING COLLEGE

Civil Services Examination-2013

Two mark questions and answers UNIT I BASIC CONCEPT AND FIRST LAW SVCET

Civil Services Examination-2001

Please welcome for any correction or misprint in the entire manuscript and your valuable suggestions kindly mail us

10 minutes reading time is allowed for this paper.

200 QUESTION PAPER SPECIFIC INSTRUCTIONS

SHRI RAMSWAROOP MEMORIAL COLLEGE OF ENGG. & MANAGEMENT

S.E. (Chemical) (Second Semester) EXAMINATION, 2012 HEAT TRANSFER (2008 PATTERN) Time : Three Hours Maximum Marks : 100

Civil Services Examination-1989

ECE309 THERMODYNAMICS & HEAT TRANSFER MIDTERM EXAMINATION. Instructor: R. Culham. Name: Student ID Number:

MC 405 MODEL TEST PAPER - 1 THERMAL SCIENCE & ENGINEERING. Time: Three Hours Maximum Marks: 100

ME 200 Final Exam December 14, :00 a.m. to 10:00 a.m.

ECE309 INTRODUCTION TO THERMODYNAMICS & HEAT TRANSFER. 13 June 2007

I. (20%) Answer the following True (T) or False (F). If false, explain why for full credit.

5/6/ :41 PM. Chapter 6. Using Entropy. Dr. Mohammad Abuhaiba, PE

SECOND ENGINEER REG. III/2 APPLIED HEAT

200 QUESTION PAPER SPECIFIC INSTRUCTIONS

Applied Fluid Mechanics


Elements of Mechanical Engineering

Chapter 5. Mass and Energy Analysis of Control Volumes. by Asst. Prof. Dr.Woranee Paengjuntuek and Asst. Prof. Dr.Worarattana Pattaraprakorn

QUESTION BANK UNIT-1 INTRODUCTION. 2. State zeroth law of thermodynamics? Write its importance in thermodynamics.

TankExampleNov2016. Table of contents. Layout

ANALYSIS OF GATE 2018*(Memory Based) Mechanical Engineering

Scheme G. Sample Test Paper-I


Objectives. Conservation of mass principle: Mass Equation The Bernoulli equation Conservation of energy principle: Energy equation

MAHARASHTRA STATE BOARD OF TECHNICAL EDUCATION (Autonomous) (ISO/IEC Certified) SUMMER 17 EXAMINATION

Hours / 100 Marks Seat No.

CHAPTER 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES

Where F1 is the force and dl1 is the infinitesimal displacement, but F1 = p1a1

Chapter Four fluid flow mass, energy, Bernoulli and momentum

FINAL EXAM. ME 200 Thermodynamics I, Spring 2013 CIRCLE YOUR LECTURE BELOW:

SILVER OAK COLLEGE OF ENGINEERING & TECHNOLOGY

R13. II B. Tech I Semester Regular Examinations, Jan THERMODYNAMICS (Com. to ME, AE, AME) PART- A

Thermal Energy Final Exam Fall 2002

S.E. (Chemical Engineering) (Second Semester)EXAMINATION, 2012 THERMODYNAMICS-I (2008 PATTERN) Time : Three Hours Maximum Marks : 100

SUMMER 14 EXAMINATION

THERMODYNAMICS, FLUID AND PLANT PROCESSES. The tutorials are drawn from other subjects so the solutions are identified by the appropriate tutorial.

UNIT 1 COMPRESSIBLE FLOW FUNDAMENTALS

Chapter 5. Mass and Energy Analysis of Control Volumes

Set 1. a. 100 kj/kg b. 110 kj/kg c. 140 kj/kg d. 150 kj/kg

Department of Mechanical Engineering Indian Institute of Technology New Delhi II Semester MEL 140 ENGINEERING THERMODYNAMICS

THE FIRST LAW APPLIED TO STEADY FLOW PROCESSES

ME 316: Thermofluids Laboratory

Readings for this homework assignment and upcoming lectures

Set 2 (d) 150 C (a) 0.45 (d) can be positive, negative or zero (C) 8.5 J/K (a) 0.1

NATIONAL CERTIFICATE (VOCATIONAL) APPLIED ENGINEERING TECHNOLOGY NQF LEVEL 4 NOVEMBER 2009

UNIFIED ENGINEERING Fall 2003 Ian A. Waitz

Q. 1 Q. 25 carry one mark each.

Section A 01. (12 M) (s 2 s 3 ) = 313 s 2 = s 1, h 3 = h 4 (s 1 s 3 ) = kj/kgk. = kj/kgk. 313 (s 3 s 4f ) = ln

SILVER OAK COLLEGE OF ENGINEERING & TECHNOLOGY ADITYA SILVER OAK INSTITUTE OF TECHNOLOGY

12/21/2014 7:39 PM. Chapter 2. Energy and the 1st Law of Thermodynamics. Dr. Mohammad Suliman Abuhaiba, PE

CHAPTER 8. Testing of I.C.Engines

Propulsion Thermodynamics

MAE 320 HW 7B. 1e. For an isolated system, please circle the parameter which will change with time. (a) Total energy;

20 m neon m propane. g 20. Problems with solutions:

SATHYABAMA UNIVERISTY. Unit III

UBMCC11 - THERMODYNAMICS. B.E (Marine Engineering) B 16 BASIC CONCEPTS AND FIRST LAW PART- A

PTT 277/3 APPLIED THERMODYNAMICS SEM 1 (2013/2014)

Refrigeration. 05/04/2011 T.Al-Shemmeri 1

Contents. 2 Basic Components Aerofoils Force Generation Performance Parameters xvii

Answers to questions in each section should be tied together and handed in separately.

Thermodynamics I Spring 1432/1433H (2011/2012H) Saturday, Wednesday 8:00am - 10:00am & Monday 8:00am - 9:00am MEP 261 Class ZA

Exam 3. Feb 12, Problem 1 / 32 Problem 2 / 33 Problem 3 / 32 Total / 100

II/IV B.Tech (Regular) DEGREE EXAMINATION. (1X12 = 12 Marks) Answer ONE question from each unit.

SHRI RAMSWAROOP MEMORIAL COLLEGE OF ENGG. & MANAGEMENT B.Tech. [SEM V (ME-51, 52, 53, 54)] QUIZ TEST-1 (Session: )

Theoretical & Derivation based Questions and Answer. Unit Derive the condition for exact differentials. Solution:

ME 2322 Thermodynamics I PRE-LECTURE Lesson 23 Complete the items below Name:

7. Development of the 2nd Law

first law of ThermodyNamics

3. Write a detailed note on the following thrust vector control methods:

Unit Workbook 2 - Level 5 ENG U64 Thermofluids 2018 UniCourse Ltd. All Rights Reserved. Sample

Fluid Mechanics Answer Key of Objective & Conventional Questions

In the next lecture...

1) Specific Gravity It is the ratio of specific weight of fluid to the specific weight of water.

ME Thermodynamics I. Lecture Notes and Example Problems

Jet Aircraft Propulsion Prof. Bhaskar Roy Prof. A.M. Pradeep Department of Aerospace Engineering

Introduction CHAPTER Prime Movers. 1.2 Sources of Energy

FE Fluids Review March 23, 2012 Steve Burian (Civil & Environmental Engineering)

Teaching schedule *15 18

SPC 407 Sheet 5 - Solution Compressible Flow Rayleigh Flow

For example an empty bucket weighs 2.0kg. After 7 seconds of collecting water the bucket weighs 8.0kg, then:

3 Energy Exchange in Turbomachines

Hydraulic modeling assessment Copyright 2010, Optimized Technical Solutions, LLC

SHORTCUT CALCULATIONS AND GRAPHICAL COMPRESSOR SELECTION PROCEDURES

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

PHYA5/2C. (JUN15PHYA52C01) WMP/Jun15/PHYA5/2C/E5. General Certificate of Education Advanced Level Examination June Section B PMT TOTAL

Mathematical Modelling for Refrigerant Flow in Diabatic Capillary Tube

Principles of Food and Bioprocess Engineering (FS 231) Problems on Heat Transfer

Heat and Mass Transfer Unit-1 Conduction

BACHELOR OF TECHNOLOGY IN MECHANICAL ENGINEERING (COMPUTER INTEGRATED MANUFACTURING)

INSTITUTE OF AERONAUTICAL ENGINEERING (Autonomous) Dundigal, Hyderabad

Transcription:

Roll No. Candidate should write his/her Roll No. here. Total No. of Questions : 7 No. of Printed Pages : 8 SEM-2016(03)-II MECHANICAL ENGINEERING Paper -11 Time : 3 Hours ] [ Total Marks : 300 Instructions to the candidates: Please read each of the following instructions carefully before attempting questions. Candidate should attempt FIVE questions in all. Question No. 1 is compulsory. The remaining FOUR questions are to be attempted by selecting anyfour out ofthese six questions Q2 to Q7. All questions carry equal marks. The number ofmarks carried by a part of a question is indicated against it. Answer must be written in ENGLISH only. Unless otherwise mentioned, symbols and notations have their usual standard meanings. Assume suitable data, ifnecessary and indicate the same clearly. Neat sketches may be drawn, wherever required. All parts and sub-parts ofa question are to be attempted together in the answer book. Any pages left blank in the answer book must be clearly struck out. P.T.O.

I. (a) Find the heat transferred to a gas of 2 kg when it is heated from 20 C to ICQ C. The specific heat of gas at constant volume is given by C =(0.5 + 0.005 T) kj/kg C also find out the mean value of specific heat. (b) A stone of mass 10 kg and tank containing 100 kg water are initially at same temperature. A stone above 100 m falls into the water. Considering the stone and water as a system, determine AU, APE, AKE ^ and W, when (i) the stone is about to enter the water (ii) the stone has come to rest in the tank. (c) In a flowing river a body is immersed at a depth of 3.5 m and the pressure on the upstream face of the body is found to be 35.30 kn/m^. Find the velocity of the river at that depth. u y (d) If the velocity distribution in the boundary layer is given by ~ = 'r, V s determine the displacement thickness, the momentum thickness and the energy thickness.

(e) The temperature distribution across a wall 1 m thick at a certain instant of time is given by T(;c) = a + hx + while a = 900 C, b = -300 C/m and C = -50 X/m^. A uniform heat generation q = 1000 W/m^ is present in the wall area of 10 having the property K = 40 W/m K. Determine the rate of heat transfer entering the wall (x = 0) and leaving the wall (x = 1 m). Also calculate the rate of change of energy storage in wall. (f) A system for heating water from an inlet temperature of 20 to an outlet temperature of 60 C involves passing the water through a thick walled tube having inner and outer diameters of 20 and 40 mm. The outer surface of the tube is well insulated and electrical heating within the wall provides for a uniform generation of heat of q = 10^ W/m^. For a water mass flow rate of m = 0.1 kg/s, how long must the tube be to achieve the desired outlet temperature? Take C =4179 J/kg K. (g) An engine working on otto-cycle has a volume of 0.5 m^ pressure 1 bar and temperature of 27 C at the beginning of the compression stroke. At the end of the compression stroke, the pressure is 10 bar, 210 kj of heat is added during constant volume heating process. Calculate the pressures. temperatures and volumes at salient points in the cycle. P.T.O.

(h) For a vapour compression refrigeration system, sketch p-h diagram on T-S diagram and express the coefficient of performance of the cycle in terms of enthalpies. (i) Explain any three geometry statements and three motion statements in APT language. (j) Explain the general application characteristics in an environment of material handling by robots. (a) Three pipes of same length L, diameter D and friction factor f are connected in parallel. Determine the diameter of the pipe of length L and friction factor f which will carry the same discharge for the same head f X L X loss. Use the formula bf = 2^^ (b) Oil with a free stream velocity of 2 m/sec flows over a thin plate 2 m wide and 2 m long. Calculate the boundary layer thickness and the shear stress at the trailing end point and determine the total surface resistance of the plate. Take specific gravity as 0.86 and kinematic viscosity as 10"^ m^/sec. (a) 0.5 kg of air, initially at 25 C is heated at constant pressure until the volume is doubled and is then heated at constant volume until the pressure is doubled. For the total path, find the work transfer, heat transfer and change in entropy.

(b) A plane wall is a composite of two materials A & B. The wall of material A has unifonn heat generation q = 1.5 x 10^ W/m^, = 75 W/m K and thickness = 50 mm. The wall material B has no generation with Kg == 150 W/m K and thickness Lg = 20 mm. The inner surface of material A is well insulated, while the outer surface of material B is cooled by a water stream with T^ = 30 C and h = 1000 W/m^ K. Determine the temperature Tq of the insulated surface and the temperature of Tj of the cooled surface. (a) Two large parallel planes having emissivities of 0.3 and 0.5 are maintained at 800 C and 350 C respectively. A radiation shield having an emissivity of 0.05 on both sides is placed between the two planes, calculate (i) heat transfer per without shield (ii) the temperature of shield and (iii) heat transfer per with shield. (b) A vapour compression cycle with ammonia as refrigerant works between the limits of saturated suction temp, of -20 and saturated condensing temp, of 30 C. It is a simple saturated cycle and compression is isentropic, determine the woric of compression per kg of ammonia. Compare the same if ammonia vapours leaving the evaporator at -20 C is absorbed by water so that the mass concentration in the solution reaches about 40% and its solution is pumped to the condenser pressure. Assume specific volume of solution to be 0.001161 m%g. Assume h2 = 1420 kj/kg and = 1668 kj/kg. (p-h chart values)

5. (a) During the test on 4-cylinder, 4-stroke petrol engine, the following readings are taken: Diameter of the cylinder = 80 mm, stroke of the piston =100 mm. Speed of the engine = 3000 rpm. Load on the hydraulic dynamometer = 160 N, Dynamometer constant = 20420 when speed is in rpm. Fuel consumption = 8 kg/hr. Cy of the fuel used = 43000 kj/kg. The temperature and pressure of the charge at the end of suction stroke = 15 C and 1 bar. A : F ratio =13: 1. For the determination of the mechanical efficiency of the engine, a Morse test was carried out by shorting the spark plugs of each cylinder successively without change of speed. The corresponding BP'S of the engine are 16.5, 16, 15.6 and 17.6 kw respectively. Determine (i) The BP, Brake mean effective pressure and Brake thermal efficiency of the engine. (ii) Also find the mechanical efficiency and volumetric efficiency of the engine at suction condition. (30 + (b) A gas turbine plant operates on Brayton cycle between temp, limit of 1100 K and 310 K. Calculate the maximum work done per kg of air (kj/kg) and corresponding cycle efficiency.

(a) A Kaplan turbine develops 24647.6 kw power at an average head of 39 metres. Assuming a speed ratio of 2, flow ratio of 0.6, diameter of the boss equal to 0.35 times the diameter of the runner and an overall efficiency of 90%. Calculate the diameter, speed and specific speed of the turbine. (b) A simple turbo-jet unit operates with a turbine inlet ten^)erature of 1100 K, a pressure ratio is 4 : 1 and air man flow of 22.7 kg/sec under design conditions. The following component efficiencies may be assumed: Isentropic compressor efficiency - 0.85 Isentropic turbine efficiency - 0.90 Propelling nozzle efficiency - 0.95 Transmission efficiency - 0.99 Combustion chamber pressure loss - 0.21 Calculate the design thrust and specific fuel consumption when the unit is stationary at sea-level where the ambient condition may be taken as 1.013 bar and 288 K Cp,= 1.0035,73,= 1.4 1-147,7^= 1.33 L.C.V. of the fuel = 43125 kj/kg K.

7. (a) Explain the working of Raster Scan (Digital TV) as a graphics terminals for CAD (b) Explain the relationship of adoptive control machining in computer aided manufacturing. (c) The work table of a positioning system is driven by a lead screw having pitch = 6 mm. The lead screw is connected to the output shaft of stepper motor through a gearbox whose ratio is 8 : 1. The stepper motor has 72 step angles. The table must move a distance of 240 nun from its present position at a linear velocity of 540 mm/min. Determine the no. of pulses required to move the table and required motor speed. 03-11(2)