An aircraft flies at Mach 1.5 at 510o00 ft (Pa=11.0KPa,Ta=216.7 K) propelled by a simple turbojet...
Fantastic news! We've Found the answer you've been seeking!
Question:
Transcribed Image Text:
An aircraft flies at Mach 1.5 at 510o00 ft (Pa=11.0KPa,Ta=216.7 K) propelled by a simple turbojet engine. The air enters the compressor and turbine at a rate of 20kg/s. (y=1.4,cp=1005J/(kg•K)). a. Find the stagnation temperature and pressure into the compressor, if the inlet is effectively isentropic. b. The engine compressor has a pressure ratio of 15 with an isentropic efficiency of 85%. Find the compressor work input. c. In the combustor the velocities are low (so the stagnation and static pressure are equal) with 5% pressure drop. At turbine entry the stagnation temperature is 1400 K and the turbine has an efficiency of 89% and 65% work output from turbine is used as compressor work input. Calculate the pressure ratio of the turbine and the thermal efficiency. d. If the final propelling nozzle is isentropic, find the velocity of the jet. An aircraft flies at Mach 1.5 at 510o00 ft (Pa=11.0KPa,Ta=216.7 K) propelled by a simple turbojet engine. The air enters the compressor and turbine at a rate of 20kg/s. (y=1.4,cp=1005J/(kg•K)). a. Find the stagnation temperature and pressure into the compressor, if the inlet is effectively isentropic. b. The engine compressor has a pressure ratio of 15 with an isentropic efficiency of 85%. Find the compressor work input. c. In the combustor the velocities are low (so the stagnation and static pressure are equal) with 5% pressure drop. At turbine entry the stagnation temperature is 1400 K and the turbine has an efficiency of 89% and 65% work output from turbine is used as compressor work input. Calculate the pressure ratio of the turbine and the thermal efficiency. d. If the final propelling nozzle is isentropic, find the velocity of the jet.
Expert Answer:
Related Book For
Thermodynamics An Engineering Approach
ISBN: 978-0073398174
8th edition
Authors: Yunus A. Cengel, Michael A. Boles
Posted Date:
Students also viewed these mechanical engineering questions
-
Air at 7C enters a turbojet engine at a rate of 16 kg/s and at a velocity of 300 m/s (relative to the engine). Air is heated in the combustion chamber at a rate 15,000 kJ/s and it leaves the engine...
-
Air at 10oC enters a turbojet engine at a rate (m) of 15 kg/s and at a velocity of 320 m/s (relative to the engine). Air is heated in the combustion chamber at a rate of 25000 kJ/s and it leaves the...
-
Air at 7C enters a turbojet engine at a rate of 16 kg/s and at a velocity of 300 m/s (relative to the engine). Air is heated in the combustion chamber at a rate 15,000 kJ/s and it leaves the engine...
-
Show that plane stress displacements for the Flamant problem in Section 8.4.7 under only tangential force X are given by: Data from section 8.4.7 My (1 v) - - -0 sin (1 v)X, -0 cost + 2X, 20 log r...
-
A horizontal, insulated cylinder has a frictionless piston held against stops by an external force of 500 kN. The piston cross-sectional area is 0.5 m2, and the initial volume is 0.25 m3. Argon gas...
-
The contribution margin income statement of Westlake Coffee for February follows: Westlake coffee sells three small coffees for every large coffee. A small coffee sells for $ 3.00, with a variable...
-
CMS is a claims processing company in Mobile, Alabama. Chastity Jones, a black woman, completed an online employment application for a customer service position with CMS. Jones interviewed with a...
-
Two Indiana state senate candidates must decide which city to visit the day before the November election. The same four citiesIndianapolis, Evansville, Fort Wayne, and South Bendare available for...
-
If the trend towards authoritarianism continues and more democracies move towards the totalitarian side of the spectrum, how could that affect the international political system?
-
Think about your school or local library and the processes involved in checking out books, signing up new borrowers, and sending out overdue notices, all from the librarys perspective. Describe three...
-
Complete the following problems using the information given below: Total Project Cost: Lender Standards: . . . . o Interest Rate: o Amortization Rate: o Debt service coverage ratio: o Debt-to-cost...
-
Explain the Amihud and Mendelson (1986) arguments for why illiquidity impacts on asset prices. Explain why stock returns are an increasing and concave function of illiquidity. Why do we observe that...
-
How is the plaintiff able to establish a prima Dixie case of desperate treatment?
-
Using inheritance, one class can acquire the properties of others. Consider the following Animal class: class Animal{ void walk(){ System.out.printIn("I am walking") ; ] A ] This class has only one...
-
What is the number one lesson when it comes to corporate finance?
-
Top Hatters sold $38.9 million worth in men's hats last year inits local market. Their largest competitor, Lidz Inc., sold $28.3million, and other firms sold $53.4 million in this market.Calculate...
-
Who were Europe s Great Powers in 1 5 0 0 ?
-
QUESTION 2 The CEO of Farisha Hijab Sdn Bhd insisted on further investigation to be carried out that he also required Mr Muaz to conduct the analysis of variance for the material and labour of the...
-
On a T-s diagram, does the actual exit state (state 2) of an adiabatic turbine have to be on the right-hand side of the isentropic exit state (state 2s)? Why?
-
Show that: av , ,
-
Steam enters an adiabatic turbine at 8 MPa and 500°C with a mass flow rate of 3 kg/s and leaves at 30 kPa. The isentropic efficiency of the turbine is 0.90. Neglecting the kinetic energy change...
-
Prove that the boosted right-handed spinor \(\psi_{\mathrm{R}}(\boldsymbol{p})\) is related to the corresponding rest spinor by Eq. (14.21).
-
Use the \(\gamma\)-matrices in the Weyl representation to show that the Dirac equation (14.31) is equivalent to Eq. (14.25). Data from Eq. 14.31 Data from Eq. 14.25 (y"Pu-m)(p) = (iy" - m)(p) = 0
-
Prove the identity \((\sigma \cdot \boldsymbol{p})^{2}=\mathrm{I}^{(2)} p^{2}\), where \(\sigma=\left(\sigma_{1}, \sigma_{2}, \sigma_{3} ight)\) are the Pauli matrices, \(\boldsymbol{p}\) is the...
Study smarter with the SolutionInn App