FUND OF AERODYNAMICS(LLF) +CONNECT (1YR)
6th Edition
ISBN: 9781265141387
Author: Anderson
Publisher: MCG
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Chapter 8, Problem 8.12P
Consider a flow with a pressure and temperature of
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Chapter 8 Solutions
FUND OF AERODYNAMICS(LLF) +CONNECT (1YR)
Ch. 8 - Consider air at a temperature of 230 K. Calculate...Ch. 8 - The temperature in the reservoir of a supersonic...Ch. 8 - At a given point in a flow, T=300K,p=1.2atm, and...Ch. 8 - At a given point in a flow, T=700R,p=1.6atm, and...Ch. 8 - Consider the isentropic flow through a supersonic...Ch. 8 - Consider the isentropic flow over an airfoil. The...Ch. 8 - The flow just upstream of a normal shock wave is...Ch. 8 - The pressure upstream of a normal shock wave is 1...Ch. 8 - The entropy increase across a normal shock wave is...Ch. 8 - The how just upstream of a normal shock wave is...
Ch. 8 - Consider a flow with a pressure and temperature of...Ch. 8 - Consider a flow with a pressure and temperature of...Ch. 8 - Repeat Problems 8.11 and 8.12 using (incorrectly)...Ch. 8 - Derive the Rayleigh Pitot tube formula, Equation...Ch. 8 - On March 16, 1990, an Air Force SR-71 set a new...Ch. 8 - In the test section of a supersonic wind tunnel, a...Ch. 8 - When the Apollo command module returned to earth...Ch. 8 - The stagnation temperature on the Apollo vehicle...Ch. 8 - Prove that the total pressure is constant...
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- Oil at 60 degrees celsius and 140 bars is flowing through a pressure relief valve at 0.01 m3/s. What is the downstream temperature? Show your work.arrow_forwardNatural gas, which is essentially methane is being pumped through a 1m ID steel pipe for a distance of 100 km at a rate of 2 kmol/s. It can be assumed that the flow is isothermal at 289 K. The pressure at the end of the line is 170 kPa. Assuming that the viscosity of the gas is 1.08963x10-5 Pa-s, calculate the pressure (kPa) at the pump discharge.arrow_forwardFluid is moving at rate of 3m/s in a chamber of a 12inch positive displacement flow meter, if the density of the fluid is 4.5kg/m³ and has a mass flow rate of 8kg/s, what is the maximum volume capacity of the chamber?arrow_forward
- Fluid A is three times denser than Fluid B through the same horizontal pipes. Which will flow faster? How many times faster will it be? Please show a simple equation to discuss the answer.arrow_forward4. Determine the pressure required, in psi, in the pipe just ahead of the nozzle shown in the figure to produce a jet velocity of 75 fps. The fluid is water at 180 F. * 1.0-in diameter Flow 0.75-in diameterarrow_forwardA 500 mm diameter pipe gradually reduces to 20 mm diameter and the gradually enlarge to its original size. Given the pressure at the base of the convergence of 0.60 MPa with a flow of 0.08 cu. m/s, 1. What is the velocity at point 1? 2. What is the velocity head at point 2? 3. Neglecting the head loss, the pressure of the smallest section is?arrow_forward
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- An in-compressible ideal fluid flows at 15L/s through a circular pipe into a conically converging nozzle. Determine the average velocity of flow at sections A and B of the figure below.arrow_forwardAir at standard atmospheric condition flows through a pipe at a velocity of 20 m/s, which then narrows down to smaller size. The velocity at the throat becomes 45 m/s. What is the difference between the pressures at two points?arrow_forwardWater flows steadily through a pipe with ID 35 mm. This pipe expands suddenly to an inner diameter of 75 mm and then stays at that diameter. The flow speed in the 35 mm pipe is 32 m/s. The water gage pressure in the thinner pipe is 510 kPa. 1. What is the pressure at the entrance to the thicker section of the pipe? Is the pressure there larger or smaller than in the thin pipe section?arrow_forward
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