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ISA 1932 Conical nozzle shape diffuser Throat tap 1es 15° 0.7d 2 Flow (c)

Principles of Heat Transfer (Activate Learning with these NEW titles from Engineering!)

8th Edition

ISBN:9781305387102

Author:Kreith, Frank; Manglik, Raj M.

Publisher:Kreith, Frank; Manglik, Raj M.

Chapter5: Analysis Of Convection Heat Transfer

Section: Chapter Questions

Problem 5.4P: 5.4 Evaluate the Stanton number for flow over a tube from the following data: , , , , .

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Question

Consider the venturi nozzle of Fig. , with D = 5 cm
and d = 3 cm. Stagnation temperature is 300 K, and the
upstream velocity V₁ = 72 m/s. If the throat pressure is
124 kPa, estimate, with isentropic flow theory, (a) p₁,
(b) Ma₂, and (c) the mass flow.

ISA 1932
Conical
nozzle shape
diffuser
Throat tap
1es 15°
0.7d
2
Flow
(c)

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