Mechanical Engineering 2023 Paper II 50 marks Calculate

Q8

(a) An SI engine working on the Otto cycle has cylinder bore of 210 mm and stroke length of 240 mm. The clearance volume is 1550 cc. The pressure and temperature at the beginning of compression are 1 bar and 17 °C respectively. The maximum pressure of the cycle is 50 bar. Determine the pressure and temperature at the salient points in the cycle, the air-standard efficiency, the work done and the mean effective pressure. Show the cycle on P-v and T-s diagrams. Evaluate the fuel consumption in kg/kWh, if the calorific value of the fuel is 40 MJ/kg. Take Cp and Cv of air as 1·005 kJ/kg-K and 0·718 kJ/kg-K respectively. (b) Air flowing at the rate of 100 m³/min at 40 °C DBT and 50% RH is mixed with another stream of air flowing at the rate of 20 m³/min at 26 °C DBT and 50% RH. The mixture flows over a cooling coil whose ADP temperature is 10 °C and bypass factor is 0·2. Find the DBT and RH of air leaving the coil. If this air is supplied to an air-conditioned room, where DBT of 26 °C and RH of 50% are maintained, then calculate the (i) room sensible heat factor and (ii) coil cooling capacity in tons of refrigeration. Draw a schematic diagram of the system and show all the processes on a skeleton psychrometric chart. Psychrometric chart is given. (c) A process industry employs a medium pressure boiler to produce steam. The mass flow rate of fuel consumed is 0·847 kg/s and c.v. of the fuel is 44 MJ/kg. For efficient combustion, 16 kg of air per kg of fuel is required, for which a draught of 30 mm of the water column is required at the base of the chimney. The flue gases leave the boiler at 350 °C. The average temperature of gases in the stack may be taken as 300 °C. The atmosphere is at 20 °C. Assuming the velocity of gases at the stack exit to be negligible, determine the height of the stack and the diameter at its base. Also, calculate the mass flow rate of the gases. Take Patmosphere = 101·3 kPa, Rair = Rgases = 0·287 kJ/kg-K, g = 9·81 m/s², ρwater = 1000 kg/m³.

हिंदी में प्रश्न पढ़ें

(a) ओटो चक्र पर कार्य करने वाले एक स्पार्क इग्निशन इंजन में सिलिंडर बोर 210 mm और स्ट्रोक लंबाई 240 mm है। अवकाश आयतन 1550 cc है। संपीडन के आरंभ में दाब और तापमान क्रमशः 1 bar और 17 °C है। चक्र का अधिकतम दाब 50 bar है। चक्र के मुख्य बिंदुओं पर दाब और तापमान, वायु-मानक दक्षता, कृतकार्य तथा माध्य प्रभावी दाब निर्धारित कीजिए। चक्र को P-v और T-s आरेख पर दर्शाइए। यदि ईंधन का उष्मीय मान 40 MJ/kg है, तो kg/kWh में ईंधन की खपत का मूल्यांकन कीजिए। वायु के Cp और Cv को क्रमशः 1·005 kJ/kg-K और 0·718 kJ/kg-K लीजिए। (b) 40 °C डी० बी० टी० और 50% आर० एच० पर 100 m³/min की दर से प्रवाहित वायु को 26 °C डी० बी० टी० और 50% आर० एच० पर 20 m³/min की दर से प्रवाहित वायु की दूसरी धारा के साथ मिलाया जाता है। मिश्रण शीतलन कुंडली पर से प्रवाहित होता है जिसका ए० डी० पी० तापमान 10 °C तथा उपमार्ग गुणक 0·2 है। कुंडली से निकलने वाली वायु का डी० बी० टी० और आर० एच० ज्ञात कीजिए। यदि यह वायु एक वातानुकूलित कक्ष में आपूर्ति की जाती है, जहाँ डी० बी० टी० 26 °C और आर० एच० 50% बनाए रखा जाता है, तो गणना कीजिए (i) कक्ष संवेदी उष्मा गुणक तथा (ii) प्रशीतन टन में कुंडली शीतलन क्षमता। तंत्र का एक योजनाबद्ध आरेख बनाइए और सभी प्रक्रियाओं को एक साइक्रोमीट्रिक चार्ट के ढाँचे पर दर्शाइए। साइक्रोमीट्रिक चार्ट दिया हुआ है। (c) एक प्रक्रम उद्योग भाप का उत्पादन करने हेतु एक मध्यम दाब वाले बॉयलर का उपयोग करता है। उपभोग किए गए ईंधन की द्रव्यमान प्रवाह दर 0·847 kg/s है और ईंधन का उष्मीय मान (CV) 44 MJ/kg है। कुशल दहन हेतु, प्रति kg ईंधन में 16 kg वायु की आवश्यकता होती है, जिसके लिए चिमनी के आधार पर जल स्तंभ के 30 mm के प्रवात की आवश्यकता होती है। फ्लू गैस बॉयलर से 350 °C पर निकलती है। स्टैक में गैस का औसत तापमान 300 °C लिया जा सकता है। वातावरण 20 °C पर है। यह मानते हुए कि स्टैक के निर्गम पर गैसों का वेग नगण्य है, स्टैक की ऊँचाई और उसके आधार का व्यास निर्धारित कीजिए। इसके अलावा, गैसों की द्रव्यमान प्रवाह दर की भी गणना कीजिए। Pवायुमंडल = 101·3 kPa, Rवायु = Rगैस = 0·287 kJ/kg-K, g = 9·81 m/s², ρजल = 1000 kg/m³ लीजिए।

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How this answer will be evaluated

Approach

Calculate systematically across all three sub-parts: spend ~40% time on (a) Otto cycle (highest computational load with multiple salient points, efficiency, work, MEP and fuel consumption), ~35% on (b) psychrometric mixing and cooling coil analysis (requires chart reading and bypass factor application), and ~25% on (c) chimney draught and stack design (natural draught formula with temperature-dependent density). Present each part with clear headings, state assumptions, show all formulae with substitutions, and conclude with labelled diagrams as demanded.

Key points expected

  • Part (a): Compression ratio r = (V_s + V_c)/V_c = 6.32; T2 = 562 K, p2 = 12.6 bar; T3 = 2233 K after heat addition; T4 = 1125 K, p4 = 3.97 bar; η_otto = 51.1%; W_net = 287 kJ/kg; MEP = 4.52 bar; fuel consumption = 0.202 kg/kWh
  • Part (b): Mixing line on psychrometric chart yields mixture at ~37°C DBT, 50% RH; after cooling coil with BPF=0.2, outlet DBT = 15.4°C, RH ~95%; room SHF = 0.82; coil cooling capacity = 8.6 TR
  • Part (c): Chimney height H = 42.3 m using draught equation Δp = gH(ρ_a - ρ_g); base diameter D = 1.85 m from continuity with mass flow; mass flow rate of flue gases = 14.4 kg/s
  • P-v and T-s diagrams for Otto cycle with all four states labelled and heat/work arrows indicated; skeleton psychrometric chart showing mixing, cooling coil process, and room condition line
  • Correct application of isentropic relations pV^γ = constant and T2/T1 = (V1/V2)^(γ-1) for Otto cycle; use of psychrometric relations ω = 0.622p_v/(p-p_v) and bypass factor definition
  • Unit consistency throughout: pressures in bar or kPa, temperatures in K for calculations, specific volumes in m³/kg, mass flow rates in kg/s or kg/min as appropriate

Evaluation rubric

DimensionWeightMax marksExcellentAveragePoor
Concept correctness20%2Correctly applies isentropic process relations for Otto cycle (a), uses psychrometric chart principles and bypass factor correctly for coil analysis (b), and applies natural draught equation with proper temperature-dependent gas densities for chimney (c); identifies γ = Cp/Cv = 1.4 for air.Uses correct basic formulae but makes minor errors in applying isentropic exponent or confuses BPF with contact factor; draught equation correct but uses atmospheric density instead of average stack temperature for gas density.Treats Otto cycle as Diesel cycle or uses wrong compression ratio formula; confuses DBT with WBT in psychrometrics; applies Bernoulli instead of hydrostatic draught equation for chimney.
Numerical accuracy20%2All salient point values within 2% of expected: T2≈562K, T3≈2233K, T4≈1125K, η≈51%, MEP≈4.5 bar; mixture condition and coil outlet within chart precision; chimney height ≈42m, diameter ≈1.8m; fuel consumption 0.20-0.21 kg/kWh.Correct methodology but arithmetic slips leading to 5-10% deviation in key values; correct final answers for some parts but errors in intermediate states affecting subsequent calculations.Order-of-magnitude errors (e.g., T3 in hundreds instead of thousands K); wrong compression ratio leading to completely wrong efficiency; chimney height off by factor of 2 or more.
Diagram quality20%2Clear P-v and T-s diagrams for Otto cycle with all four states labelled, isentropic curves shown, heat addition and rejection indicated; neat psychrometric skeleton showing mixing point M, cooling coil process line to ADP and outlet, room condition R; schematic of AC system with components labelled.Diagrams present but missing labels for some states or incorrect curve shapes (e.g., straight lines instead of curves for isentropes); psychrometric chart shows processes but mixing point approximate.No diagrams despite explicit demand; or diagrams drawn without any labels; or completely wrong diagrams (e.g., Diesel cycle instead of Otto cycle).
Step-by-step derivation20%2Shows all formulae with symbols first, then numerical substitution: swept volume calculation, compression ratio, isentropic relations with γ=1.4; psychrometric property calculations with steam table interpolation; draught equation derived from hydrostatic pressure balance with density as p/RT.Shows key steps but skips some intermediate derivations (e.g., jumps from T2 to T3 without showing heat addition calculation); some formulae quoted without derivation.Final answers only with no working; or working so disorganized that logic cannot be followed; missing critical steps like unit conversions or temperature conversions.
Practical interpretation20%2Comments on practical significance: for (a) compares η_otto≈51% with real SI engine efficiency (~25-30%) due to losses; for (b) notes high humidity at coil outlet and need for reheat; for (c) discusses stack thermal efficiency and pollution dispersion implications for Indian industrial boilers.Brief mention of practical relevance for one part but not others; or generic statements without specific connection to calculated values.No interpretation; treats entire problem as abstract mathematics with no engineering context; fails to note that calculated fuel consumption is idealized vs actual.

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