Fox and McDonald's Introduction to Fluid Mechanics
9th Edition
ISBN: 9781118912652
Author: Philip J. Pritchard, John W. Mitchell
Publisher: WILEY
expand_more
expand_more
format_list_bulleted
Concept explainers
Textbook Question
Chapter 12, Problem 24P
A photograph of a bullet shows a Mach angle of 32°. Determine the speed of the bullet for standard air.
Expert Solution & Answer
Want to see the full answer?
Check out a sample textbook solutionStudents have asked these similar questions
QUESTION 1
A jet of freshwater strikes a series of vanes of a turbine at 25° with the direction of
motion and leaves it at 150° absolute with the direction of motion. The absolute inlet
velocity of the jet is 25 m/s and the vanes move at a velocity of 10 m/s. Ignore friction
across the vanes. Calculate:
1.1 the vane inlet angle.
1.2 the vane outlet angle.
1.3 the power/kg of water and,
1.4 the hydraulic efficiency.
QUESTION 2
A pipeline of 50 mm diameter and 4.5 km length connects two reservoirs whose
constant difference of water level is 12 m. A branch pipe 1.25 km long and taken from
a point distance of 1.5 km from reservoir A, leads to reservoir C whose water level is
15 m below that of reservoir A. Find the diameter of the branch pipe so that the flow
into both the reservoirs is the same. Assume the coefficient of friction for each pipe,
f = 0.0075, and neglect minor losses.
QUESTION 3
The plunger diameter of a single-acting reciprocating pump is 115 mm and the stroke
is 230 mm.…
3. Calculate the speed ratio, S, for a satellite moving at 8 km/s, assuming that the ambient atmospheric species is 79 % molecular nitrogen, 21 % O2, and the temperature of the gas is 300 K. Re-do the calculation for a gas temperature of 3,000 K.
An airplane approaches at an altitude of 10 km flying at 600 km/hr.
1. What would you hear, and when would you hear it, if the plane were "hypersonic", traveling three times the speed of sound, or "Mach 3"? That's approximately the fastest military aircraft in routine service today.
note: To have higher speeds in the air takes considerably more energy. For example, after two and half minutes of flight, when the first-stage main engines of the Space X Falcon shut down, it is 80 kilometers high and moving at Mach 10 on its way to Earth orbit. The Mach number depends on the temperature of the air.
Chapter 12 Solutions
Fox and McDonald's Introduction to Fluid Mechanics
Ch. 12 - Air is expanded in a steady flow process through a...Ch. 12 - Five kilograms of air is cooled in a closed tank...Ch. 12 - Air is contained in a piston-cylinder device. The...Ch. 12 - Calculate the power delivered by the turbine per...Ch. 12 - If hydrogen flows as a perfect gas without...Ch. 12 - A 1-m3 tank contains air at 0.1 MPa absolute and...Ch. 12 - Air enters a turbine in steady flow at 0.5 kg/s...Ch. 12 - Natural gas, with the thermodynamic properties of...Ch. 12 - Carbon dioxide flows at a speed of 10 m/s in a...Ch. 12 - In an isothermal process, 0.1 cubic feet of...
Ch. 12 - Calculate the speed of sound at 20C for (a)...Ch. 12 - An airplane flies at 550 km/hr at 1500 m altitude...Ch. 12 - Actual performance characteristics of the Lockheed...Ch. 12 - For a speed of sound in steel of 4300 m/s,...Ch. 12 - Determine and plot the Mach number of an...Ch. 12 - Investigate the effect of altitude on Mach number...Ch. 12 - The grandstand at the Kennedy Space Center is...Ch. 12 - Use data for specific volume to calculate and plot...Ch. 12 - An object traveling in atmospheric air emits two...Ch. 12 - An object traveling in atmospheric air emits two...Ch. 12 - While at the seashore, you observe an airplane...Ch. 12 - The temperature varies linearly from sea level to...Ch. 12 - Prob. 23PCh. 12 - A photograph of a bullet shows a Mach angle of 32....Ch. 12 - An F-4 aircraft makes a high-speed pass over an...Ch. 12 - All aircraft passes overhead at 3 km altitude. The...Ch. 12 - A supersonic aircraft flies at 3 km altitude at a...Ch. 12 - For the conditions of Problem 12.27, find the...Ch. 12 - The Concorde supersonic transport cruised at M =...Ch. 12 - Plot the percentage discrepancy between the...Ch. 12 - Compute the air density in the undisturbed air and...Ch. 12 - Carbon dioxide flows in a duct at a velocity of 90...Ch. 12 - If nitrogen at 15C is flowing and the stagnation...Ch. 12 - An aircraft cruises at M = 0.65 at 10 km altitude...Ch. 12 - High-speed aircraft use air data computers to...Ch. 12 - A supersonic wind tunnel test section is designed...Ch. 12 - Oxygen flows in a passage at a pressure of 25...Ch. 12 - What is the pressure on the nose of a bullet...Ch. 12 - Prob. 39PCh. 12 - Air flows in an insulated duct. At point the...Ch. 12 - Consider steady, adiabatic flow of air through a...Ch. 12 - Air passes through a normal shock in a supersonic...Ch. 12 - A Boeing 747 cruises at M = 0:87 at an altitude of...Ch. 12 - Space debris impact is a real concern for...Ch. 12 - A CO2 cartridge is used to propel a toy rocket....Ch. 12 - Nitrogen flows from a large tank, through a...Ch. 12 - Air flows from the atmosphere into an evacuated...Ch. 12 - Oxygen discharges from a tank through a convergent...Ch. 12 - The hot gas stream at the turbine inlet of a JT9-D...Ch. 12 - Carbon dioxide discharges from a tank through a...Ch. 12 - Air at 100F and 100 psia in a large tank flows...Ch. 12 - Calculate the required diameter of a convergent...Ch. 12 - Steam flows steadily and isentropically through a...Ch. 12 - Nitrogen flows through a diverging section of duct...Ch. 12 - At a section in a passage, the pressure is 30...Ch. 12 - In a given duct flow M = 2.0; the velocity...Ch. 12 - Air flows isentropically through a converging...Ch. 12 - Five pounds of air per second discharge from a...Ch. 12 - Air flows isentropically through a...Ch. 12 - Air, at an absolute pressure of 60.0 kPa and 27C,...Ch. 12 - Carbon dioxide flows from a tank through a...Ch. 12 - A convergent-divergent nozzle of 50-mm tip...Ch. 12 - Air flows adiabatically through a duct. At the...Ch. 12 - Air flows isentropically through a converging...Ch. 12 - Air flows isentropically through a converging...Ch. 12 - Atmospheric air at 98.5 kPa and 20C is drawn into...Ch. 12 - The exit section of a convergent-divergent nozzle...Ch. 12 - Air flowing isentropically through a converging...Ch. 12 - Air flows from a large tank at p = 650 kPa...Ch. 12 - A converging nozzle is connected to a large tank...Ch. 12 - Air at 0C is contained in a large tank on the...Ch. 12 - A large tank initially is evacuated to 10 kPa...Ch. 12 - Air flows isentropically through a converging...Ch. 12 - Air enters a converging-diverging nozzle at 2 MPa...Ch. 12 - Prob. 75PCh. 12 - A jet transport aircraft, with pressurized cabin,...Ch. 12 - A converging-diverging nozzle, with a throat area...Ch. 12 - Air, at a stagnation pressure of 7.20 MPa absolute...Ch. 12 - A small rocket motor, fueled with hydrogen and...Ch. 12 - Testing of a demolition explosion is to be...Ch. 12 - A total-pressure probe is placed in a supersonic...Ch. 12 - Air flows steadily through a long, insulated...Ch. 12 - Air discharges through a convergent-divergent...Ch. 12 - A normal shock wave exists in an airflow. The...Ch. 12 - Air approaches a normal shock at V1 = 900 m/s, p1...Ch. 12 - Air approaches a normal shock at M1 = 2.5, with...Ch. 12 - Air undergoes a normal shock. Upstream, T1 = 35C,...Ch. 12 - If, through a normal shock wave in air, the...Ch. 12 - The stagnation temperature in an airflow is 149C...Ch. 12 - A supersonic aircraft cruises at M = 2.2 at 12 km...Ch. 12 - The Concorde supersonic transport flew at M = 2.2...
Additional Engineering Textbook Solutions
Find more solutions based on key concepts
If the allowable bending stress is allow = 22 ksi and the allowable shear stress is allow =12 ksi, select the l...
Mechanics of Materials (10th Edition)
If it has a constant speed of 75 ft/s, determine the x and y components of the vans velocity and acceleration w...
Engineering Mechanics: Dynamics (14th Edition)
Determine the moment associated with the pair of 400-N forces applied to the T-shaped structure.
Engineering Mechanics: Statics
What parts are included in the vehicle chassis?
Automotive Technology: Principles, Diagnosis, and Service (5th Edition)
5.1 through 5.7 Calculate the forces in all members of the trusses shown, using the method of joints.
Applied Statics and Strength of Materials (6th Edition)
What parts are included in the vehicle chassis?
Automotive Technology: Principles, Diagnosis, And Service (6th Edition) (halderman Automotive Series)
Knowledge Booster
Learn more about
Need a deep-dive on the concept behind this application? Look no further. Learn more about this topic, mechanical-engineering and related others by exploring similar questions and additional content below.Similar questions
- The pressure altimeter is an aneroid barometer that measures the pressure of the atmosphere at the level where the altimeter is located. Consider a jet airliner moving at 447 mph in a direction 60 degrees cast of north, has a speed relative to the ground of 503 mph due east. Recall from physics I that a plane has both an absolute speod relative to the ground, and a speed relative to the air. The values are different in the presence of wind. Draw a cartesian vector diagram of the jet, both with respect to the Earth and ait. a) Caleulate thex and y components of the geostrophic wind the plane is flying in. Use 3 sig figs for all. b) If the pilot simply flies along the pressure surface, calculate the rate of change in altitude of the plane using the characteristic Coriolis parameter defined in clas Vg x: type your answer. Vg y: type your answer. Rate of change of altitude (in m/km): type your answerarrow_forwardProvide average and instantaneous velocities formulas.arrow_forward31. Find the altitude of a supersonic airplane (T = - 52 C°, v = 730 m-s) when the time between seeing above observer and hearing is 9.3 sec.arrow_forward
- A bullet is fired with muzzle veloity of 600 m/s. If the length of the barrel is 750 mm. What is the average acceleration?arrow_forward15. Determine the aircraft Mach no. flies with the same Mach no. at elevations of 8100m (T =-44 C°) and 11000 m (T=-56 C°), if the aircraft flies 33 m- s1 slower at 11000 m altitude. daro yg ügu>arrow_forwardFind: (a) Determine the acceleration of block P. (b) Determine the friction force acting on P. Vrel P W, a Horizontal Plane (hint: Chapter 3 Acceleration-moving reference frame) Given the following: Mass of the particle m=2.4 kg, w=6 rad/s, a=4.5 rad/s^2, Vrel =6.2 m/s, Hs =0.6, µk=0.2, L=0.4 m, and h=2.3 m, What is the i component of the Normal force on particle P? What is the component of the friction force in the j direction on the particle? Answer: Checkarrow_forward
- 3 liter per 26 sec is discharged from nozzle to impact 60°target if the distance between nozzle and target equal four times a nozzle's diameter and the diameter for nozzle equal 1cm depend on this information to answer following questions: 1. determine the velocity at nozzle 2. determine the impact force 3. if we change the target to hemispherical, determine the ration between two forcesarrow_forwardi. Find the Mach no. of an aircraft flies with the same Mach no. at elevations of 8000m (T=-42 C°) and 12000 m (T =-55 C°), if the aircraft flies 30 m- s1 slower at 12000 m altitude.arrow_forwardThe jet plane in (Figure 1) is traveling at a constant speed of 1000 ft/s along the curve y = 40(10-6)? + 5000, where a and y are in feet. The pilot has a weight of 180 lb.arrow_forward
- I think 96 is the right answer.arrow_forwardPlease show the complete step-by-step solution. Choose the answer from the choices below. I’ll rate you with an upvote later. Thank you.arrow_forwardSparky needs to design a device that accelerates air in order to keep some the inflatable eagle fully inflated for some university events. The velocity through the device (V) is linear (ax + b, where a and b are constants). Since the inflatable is used on top of the ski/tubing run at Snowflex the wind velocity entering the device at x1 of 0 (V1) is 10 m/sec. Sparky needs the velocity at the exit of the 1 m-long (x2) device to be 25 m/sec (V2). For force calculations Sparky needs to know the local acceleration, convective acceleration, and total acceleration at the device inlet (x1 = 0 m) and exit (x2 = 1 m). What are these values?arrow_forward
arrow_back_ios
SEE MORE QUESTIONS
arrow_forward_ios
Recommended textbooks for you
- Elements Of ElectromagneticsMechanical EngineeringISBN:9780190698614Author:Sadiku, Matthew N. O.Publisher:Oxford University PressMechanics of Materials (10th Edition)Mechanical EngineeringISBN:9780134319650Author:Russell C. HibbelerPublisher:PEARSONThermodynamics: An Engineering ApproachMechanical EngineeringISBN:9781259822674Author:Yunus A. Cengel Dr., Michael A. BolesPublisher:McGraw-Hill Education
- Control Systems EngineeringMechanical EngineeringISBN:9781118170519Author:Norman S. NisePublisher:WILEYMechanics of Materials (MindTap Course List)Mechanical EngineeringISBN:9781337093347Author:Barry J. Goodno, James M. GerePublisher:Cengage LearningEngineering Mechanics: StaticsMechanical EngineeringISBN:9781118807330Author:James L. Meriam, L. G. Kraige, J. N. BoltonPublisher:WILEY
Elements Of Electromagnetics
Mechanical Engineering
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Oxford University Press
Mechanics of Materials (10th Edition)
Mechanical Engineering
ISBN:9780134319650
Author:Russell C. Hibbeler
Publisher:PEARSON
Thermodynamics: An Engineering Approach
Mechanical Engineering
ISBN:9781259822674
Author:Yunus A. Cengel Dr., Michael A. Boles
Publisher:McGraw-Hill Education
Control Systems Engineering
Mechanical Engineering
ISBN:9781118170519
Author:Norman S. Nise
Publisher:WILEY
Mechanics of Materials (MindTap Course List)
Mechanical Engineering
ISBN:9781337093347
Author:Barry J. Goodno, James M. Gere
Publisher:Cengage Learning
Engineering Mechanics: Statics
Mechanical Engineering
ISBN:9781118807330
Author:James L. Meriam, L. G. Kraige, J. N. Bolton
Publisher:WILEY
Dynamics - Lesson 1: Introduction and Constant Acceleration Equations; Author: Jeff Hanson;https://www.youtube.com/watch?v=7aMiZ3b0Ieg;License: Standard YouTube License, CC-BY