Fox And Mcdonald's Introduction To Fluid Mechanics
9th Edition
ISBN: 9781118921876
Author: Pritchard, Philip J.; Leylegian, John C.; Bhaskaran, Rajesh
Publisher: WILEY
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Textbook Question
Chapter 7, Problem 52P
A model hydrofoil is to be tested at 1:20 scale. The test speed is chosen to duplicate the Froude number corresponding to the 60-knot prototype speed. To model cavitation correctly, the cavitation number also must be duplicated. At what ambient pressure must the test be run? Water in the model test basin can be heated to 130°F, compared to 45°F for the prototype.
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1. A model submarine is tested in a sea water tank at a speed of 30 m/s. The prototype
speed should be 21.6 km/hr.
(a) Determine the geometric scale between the model and the prototype
(b) Determine the model speed if it is tested in a pressurized air wind tunnel with
12/s.
kinematic viscosity v = 8 × 10-7 m² /s. For sea water use v = 1.124 × 10-6 m² /s.
(e) An airplane flies at 800km/h at 11700m standard altitude where the ambient pressure
and temperature are 20.335 kPA and 216.66K respectively. A 1/50 scale model of the
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section wind speed and pressure such that force coefficients of the model and prototype are
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and compressible; equation of state for a perfect gas applies]
A light parachute for military purposes is being designed. Its diameter is 7.3 m, test load, parachute and rig weight is 1023 N. For this weight, the limit descent speed Vt = 6.1 m / s, which is taken as a basis in the design of the parachute. The 1/12 scale model will be tested in the wind tunnel and the temperature and pressure of the tunnel are the same as that of the prototype. (15.5 ºC and standard atmospheric pressure)
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b) At what speed should the wind tunnel be run to achieve dynamic similarity?
c) Calculate the aerodynamic resistance of the model parachute in the wind tunnel. Density of air at 15.5 ºC and standard atmospheric pressure ρ = 1.22 kg / m3 viscosity, µ = 8.16x10-6 kg / m.s will be taken.
Chapter 7 Solutions
Fox And Mcdonald's Introduction To Fluid Mechanics
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