Question

Air (? = 287 J / kg−?, ?? = 1005 J / kg−?, and ? =...

Air (? = 287 J / kg−?, ?? = 1005 J / kg−?, and ? = 1.4) behaves as an ideal and perfect gas and flows adiabatically and
isentropically through a duct at a velocity of 320 m/s with a pressure of 175 kPa and a temperature of 377 K. For these
conditions, determine:
a) the Mach number (Ma)
b) the stagnation temperature (To)
c) the stagnation pressure (po)
d) the stagnation density (ρo

Homework Answers

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
A) 1 kg of air with a pressure of 13 bar and a temperature of 125...
A) 1 kg of air with a pressure of 13 bar and a temperature of 125 ° C is heated as isobar up to 550 ° C. a) Work done during heating, b) Internal energy and enthalpy change, c) Calculate the amount of heat consumed. (R = 287 j / kgK, x = 1,4) B) An ideal gas with a pressure of 1 bar and a volume of 0.5m³ is compressed isothermally up to 17 bar pressure. Calculate the volume...
Pressure and temperature at the beginning of compression of compression of an air-standard (R=287 J/kgK, gamma=...
Pressure and temperature at the beginning of compression of compression of an air-standard (R=287 J/kgK, gamma= cp/cv=1.4). Diesel cycle are 107kPa and 280K, respectively. At the end of the heat addition, the pressure is 11MPa and the temperature is 2040K. a) Determine the cut off ratio:
An adiabatic gas turbine uses air to produce work. Air expands adiabatically from 600 kPa and...
An adiabatic gas turbine uses air to produce work. Air expands adiabatically from 600 kPa and 287 C to 90 kPa and 67 C. Take specific heats at room temperature (300 K). a) Find the isentropic efficiency of the turbine. b) Find the work produced by the turbine for a mass flow rate of 2.5 kg/s. c) If the mass flow rate of air is again 2.5 kg/s, find the entropy generation under steady conditions.
Let's say you completely boil 3.96 kg of rubbing alcohol at constant air pressure 99.7 kPa....
Let's say you completely boil 3.96 kg of rubbing alcohol at constant air pressure 99.7 kPa. What will be the resulting volume of vapor, in m3, assuming it behaves like an ideal gas? (Possibly useful: density of rubbing alcohol: 0.786 kg/liter, molar mass of rubbing alcohol: 60.1 kg/kmol, gas constant R = 8.314 kJ K−1 kmol−1. Beware K vs °C, Pa vs kPa, g vs kg, mol vs kmol, etc.)
Air was compressed (polytropic process) from p1= 100kPa and T1= 293Kto p2= 0.3MPa and v2=0.2803m3/kg. The...
Air was compressed (polytropic process) from p1= 100kPa and T1= 293Kto p2= 0.3MPa and v2=0.2803m3/kg. The isentropic exponent of the gas and specific gas constant are 1.4 and 287 J/(kgK), respectively. Determine (a) polytropic exponent, (b) heat and work of this process, (c) change of internal energy, (d) change of entropy of air,if mass of air is 2kgand air can be treated as ideal gas.Additionally,(e) draw the process on the p-v and T-s diagrams.You can round temperature to one decimal...
5 kg of air in a piston cylinder assembly undergoes a Carnot power cycle. Heat is...
5 kg of air in a piston cylinder assembly undergoes a Carnot power cycle. Heat is received at temperature?1=727°C and rejected at ?3=27°C.During the heat input process, the pressure changes from ?1=1200kPa to ?2=900kPa, respectively. Assume the air behaves as an ideal gas with constant specific heats. Determine: a.pressures [kPa] at beginning and end of the isothermal heat rejection process (?3,?4) b.heat transfer from high temperature source [kJ] c.thermal efficiency d.net work output for cycle [kJ]
Use cold-air-standard analysis with the fluid modeled as an ideal gas with R=0.287 kJ/kg-K and constant...
Use cold-air-standard analysis with the fluid modeled as an ideal gas with R=0.287 kJ/kg-K and constant k=1.4. Neglect changes in kinetic and potential energy. Consider a SSSF of air at 300 K and 100 kPa entering the compressor of a Simple Brayton Cycle Gas Turbine powerplant. The cycle pressure ratio is 40 and maximum cycle temperature is 1800 K. For compressor isentropic efficiency of 82% the compressor work input per unit mass = __ kJ/kg (enter the nearest positive integer...
Air with a mass of 2 kg is heated at a constant pressure of 200 kPa...
Air with a mass of 2 kg is heated at a constant pressure of 200 kPa to a temperature of 500°C. Calculate the entropy change if the initial volume is 0.8 m3. Take ???? = 1.00 kJ/kg ? K and model air as an ideal gas. (Hint: Use the appropriate TdS [Gibbs] relation to calculate entropy change.)
A turbojet aircraft is flying with a velocity of 320 m/s at a certain altitude, where...
A turbojet aircraft is flying with a velocity of 320 m/s at a certain altitude, where the ambient conditions are 32 kPa and -32°C. The pressure ratio across the compressor is 12, and the temperature at the turbine inlet is 1400K. Air enters the compressor at a rate of 40 kg/s, and the and the jet fuel has a heating value of 42700 kJ/kg. Assuming ideal operations for all components and constant specific heats for air at room temperature, (Cp=1.005...
7.2 A Brayton cycle gas engine is analyzed using the air standard method. Given the conditions...
7.2 A Brayton cycle gas engine is analyzed using the air standard method. Given the conditions at state 1, pressure ratio (rp), and cutoff ratio (rc) determine the efficiency and other values listed below. The specific heat ratio and gas constant for air is given as k=1.4 and R=0.287 kJ/kg-K respectively. T1 (K) = 333 P1 (kPa) = 170 rp = 10.7 rc = 2.54 AV (m3/s) = 1.7 a) Determine the specific enthalpy (kJ/kg) at state 1. b) Determine...