Connect with LearnSmart for Anderson: Fundamentals of Aerodynamics, 6e
6th Edition
ISBN: 9781259683268
Author: Anderson, John
Publisher: Mcgraw-hill Higher Education (us)
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Chapter 3, Problem 3.6P
A Pilot tube on an airplane flying at standard sea level reads
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Chapter 3 Solutions
Connect with LearnSmart for Anderson: Fundamentals of Aerodynamics, 6e
Ch. 3 - For an irrotational flow. show that Bernoullis...Ch. 3 - Consider a venturi with a throat-to-inlet area...Ch. 3 - Consider a venturi with a small hole drilled in...Ch. 3 - Consider a low-speed open-circuit subsonic wind...Ch. 3 - Assume that a Pitot tube is inserted into the...Ch. 3 - A Pilot tube on an airplane flying at standard sea...Ch. 3 - At a given point on the surface of the wing of the...Ch. 3 - Consider a uniform flow with velocity V. Show that...Ch. 3 - Show that a source flow is a physically possible...Ch. 3 - Prove that the velocity potential and the stream...
Ch. 3 - Prove that the velocity potential and the stream...Ch. 3 - Consider the flow over a semi-infinite body as...Ch. 3 - Derive Equation (3.81). Hint: Make use of the...Ch. 3 - Derive the velocity potential for a doublet; that...Ch. 3 - Consider the nonlifting flow over a circular...Ch. 3 - Consider the nonlifting flow over a circular...Ch. 3 - Consider the lifting flow over a circular cylinder...Ch. 3 - The lift on a spinning circular cylinder in a...Ch. 3 - A typical World War I biplane fighter (such as the...Ch. 3 - The Kutta-Joukowski theorem, Equation (3.140), was...Ch. 3 - Consider the streamlines over a circular cylinder...Ch. 3 - Consider the flow field over a circular cylinder...Ch. 3 - Prove that the flow field specified in Example 2.1...
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- The figure below shows a Venturi meter for measuring the water flow rate through a pipe. The cross-sectional area at Stations 1 and 2 is 0.01 m² and 0.006 m², respectively. The pressure difference between Stations 1 and 2 is measured using a U-tube manometer containing a liquid with a specific gravity (SG) of 1.4. The manometer head is h = 0.8 m. What is the volume flow rate Q through the pipe? Neglect viscous effects. The gravitational acceleration g is 9.81 m/s and the density of water is 1000 kg/m³. (Note: The pressure difference is NOT simply given by PMgh, where PM is the density of the manometer liquid) 0= 1 m² s 1 2 Enter the correct answer below. 1 Please enter a number for this text box.arrow_forwardThe figure below shows a Venturi meter for measuring the water flow rate through a pipe. The cross-sectional area at Stations 1 and 2 is 0.01 m² and 0.006 m², respectively. The pressure difference between Stations 1 and 2 is measured using a U-tube manometer containing a liquid with a specific gravity (SG) of 1.4. The manometer head is h = 0.5 m. What is the volume flow rate Q through the pipe? Neglect viscous effects. The gravitational acceleration g is 9.81 m/s² and the density of water is 1000 kg/m³. (Note: The pressure difference is NOT simply given by PMgh, where PM is the density of the manometer liquid.) Q= 1. [0.014113976, 0.015599657 m³/s. 1 2 IT harrow_forwardA pitot-static tube is used for measuring the air velocity, as shown in the figure below. The pitot-static tube is connected to a U- tube manometer containing a liquid of specific gravity SG = 0.9 which indicates a difference of head of H=4 cm of the liquid. What is the air velocity V? The density of water and air is 1000 kg/m³ and 1.2 kg/m³, respectively, and the gravitational acceleration g is 9.81 m/s². 1. [23.51755348, 24.97224751 m/s. V= Air Velocity V Pitot-static probe Liquid of Specific Gravity SG H 9arrow_forward
- A 118-mm-diameter pipe enlarges to a 149-mm-diameter pipe. At section 1 of the smaller pipe, the density of gas in steady flow is 264.656 kg/m3, and the velocity is 23 m/s; at section 2 of the larger pipe, the velocity is 15 m/s. Find the unit weight (in kN/m3) of the gas at section 2. Round off to three decimal places.arrow_forwardSHOW THE CORRECT AND DETAILED FIGURE OF THIS PROBLEM. ANSWER: -2.72 J/Narrow_forwardc) A nozzle is fastened to the end of a U-tube with dimensions as shown in Figure Q2c. The nozzle exhausts into atmospheric pressure at 100 kPa; neglect friction and compute the force exerted on the U-tube by the water. If the force required to hold the nozzle is 850 N, determine the inlet pressure. 5 CRN 31896 V = 1 m/s 5 cm diameter 1 cm diameter Figure Q2carrow_forward
- The altimeter on a low-speed Cessna 172 reads 8,000 ft. By an independent measurement, the outside air temperature is 505°R. If a Pitot tube mounted on the wingtip measures 1818 Ib/ft2, what is the true velocity of the airplane?arrow_forward*83. Go Two hoses are connected to the same outlet using a Y-connector, as the drawing shows. The hoses A and B have the same length, but hose B has the larger radius. Each is open to the atmosphere at the end where the water exits. Water flows through both hoses as a viscous fluid, and Poiseuille's law [Q = ™R°(P2 – P)/(8nL)] applies to each. In this law, , P, is the pressure upstream, P, is the pressure downstream, and Q is the volume flow rate. The ratio of the radius of hose B to the radius of hose A is Rg/RA = 1.50. Find the ratio of the speed of the water in hose B to the speed in hose A. Water from outlet Hose A Hose B Problem 83arrow_forwardA 300 mm by 150 mm Venturi meter (c = 0.985) carries 0.0566 m /s of water with a differential gage reading of 0.634 m. What is the specific gravity of the gage liquid?arrow_forward
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