Liquid phenol at 298 k, 100kPa is burned with 152% theoretical air at 295k, 100kPa. Determine...

Liquid phenol at 298 k, 100kPa is burned with 152% theoretical air at 295k, 100kPa. Determine the adiabatic flame temperature. Enthalpy of liquid phenol is given as -96,232 kJ/kmol

Expert Solution

samet mamat answered 9 months ago

Determine the adiabatic flame temperature when liquid octane, C8H18 at 25C is burned with 300% theoretical...

Determine the adiabatic flame temperature when liquid octane, C8H18 at 25C is burned with 300% theoretical air at 25C in a steady flow process.

One kg of Methance (CH4) is burned with 200% theoretical air. What is the air fuel...

One kg of Methance (CH4) is burned with 200% theoretical air. What is the air fuel ratio on a mass basis?

Octane is burned completely with theoretical air in a steady-flow process at a constant pressure of...

Octane is burned completely with theoretical air in a steady-flow process at a constant pressure of 100 kPa. The products of combustion are cooled to 25 C. Calculate the number of kg of H2O which will condense per kg of fuel.

200. g of liquid phase octane (C8H18) are burned in air at a temperature of 100....

200. g of liquid phase octane (C8H18) are burned in air at a temperature of 100. degrees Celsius and a pressure of 1.00 atm, forming vapor phase water and carbon dioxide. a) Write the balanced chemical reaction equation for this process. b) What is the magnitude of the difference between ΔE and ΔH for one mole of octane going through this process? (Hint: use the value of R that makes life easiest.) c) The reaction is in contact with a...

Larson (1964) measured the diffusivity of chloroform in air at 298 K and 1 atm and...

Larson (1964) measured the diffusivity of chloroform in air at 298 K and 1 atm and reported its value as 0.093 cm2/s. Estimate the diffusion coefficient by the Wilke-Lee equation and compare it with the experimental value.

Calculate the theoretical flame temperature for CO gas burned at constant pressure with 100% excess air,...

Calculate the theoretical flame temperature for CO gas burned at constant pressure with 100% excess air, when the reactants enter at 100°C. Please show work, do not copy the solution founded. show your solution! if you can not answer this question, then do not attempt to copy others' work.

Estimatethe total entropy change when 100.g of liquid water, initially at 298 K and 0.50 atm,is...

Estimatethe total entropy change when 100.g of liquid water, initially at 298 K and 0.50 atm,is first heated to boiling at 373 K and 1.00atm, and the steamcollected at 1.00 atmsubsequently heated and compressed to 500Kand20.atm. UseDHvap(at 100 ̊C, 1 atm)= 40.6 kJ/mol and the following values for the heat capacity:CP,m(H2O,l) = 75.2 J/(K mol), CP,m(H2O,g) = 35.0J/(K mol)

Use the values found in Thermodynamic Properties to determine ΔS°, ΔH° and ΔG° at 298 K...

Use the values found in Thermodynamic Properties to determine ΔS°, ΔH° and ΔG° at 298 K for the reaction below. Enter all values to the 0.1 place. 4 NH3(g) + 5 O2(g) → 4 NO(g) + 6 H2O(g) ΔS° ΔH° ΔG°

Consider the following reaction at constant P. Determine the value of ΔSsurroundings at 298 K? Predict...

Consider the following reaction at constant P. Determine the value of ΔSsurroundings at 298 K? Predict whether or not this reaction will be spontaneous at this temperature. N2(g) + 2 O2(g) → 2 NO2(g); ΔH = +66.4 kJ (Please show work and thank you for taking the time to answer.)

1. Calculate the adiabatic flame temperature for the following mixtures initially at 298 K: stoichiometric butane-air...

1. Calculate the adiabatic flame temperature for the following mixtures initially at 298 K: stoichiometric butane-air mixture, stoichiometric butane-oxygen mixture, 2.0% (by volume) of butane in air. Use enthalpies of formation and heat capacities from the NIST Chemistry WebBook, which can be found at http://webbook.nist.gov/chemistry/. 2) Repeat the adiabatic flame temperature calculation without the restriction on the possible products using an online version of the CEA calculator developed by NASA and located at http://www.grc.nasa.gov/WWW/CEAWeb/ceaHome.htm. Compare the results of the two...

Question