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See all pages
with references to "inlet stagnation pressure".
Excerpt - on Page 65: "
... Mach number at any location x along the channel, M(x), is therefore defined by the local ratio of static to inlet stagnation pressure, M(x) Y - 1 P( X) 2 ) (x) - 1 . ... "
Key Phrases:
Kelvin's Theorem, Crocco's Theorem, Divergence Theorem, Stokes's Theorem, Taylor-Proudman Theorem, stagnation pressure change, stagnation temperature distribution, boundary layer shape parameter, stagnation pressure difference, streamwise vorticity generation, lobed mixer, convected disturbances
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Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines (Cambridge Engine Technology Series)
by Nicholas A. Cumpsty
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with references to "inlet stagnation pressure".
Excerpt - on Page 59: "
... its inlet the engine rsponds to the stagnation temperature and pressure. For flight at a Mach number of 0.85 the inlet stagnation pressure is related to the ambient pressure by equation (6.5) giving p02/pa = 1.604. ... "
Key Phrases:
Rolls Royce, General Electric, compressor delivery temperature, fan pressure ratio, propelling nozzle area, inlet stagnation pressure, rotor cooling air, bet velocity, overall pressure ratio, inlet stagnation temperature, core mass flow, bypass nozzle
(see more)
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Jet Propulsion: A Simple Guide to the Aerodynamic and Thermodynamic Design and Performance of Jet Engines
by Nicholas Cumpsty
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with references to "inlet stagnation pressure".
Excerpt - on Page 63: "
... For flight at a Mach number of 0.85 the inlet stagnation pressure is related to the ambient pressure by equation (6.5) giving P02/Pa = 1.604. The flow at nozzle exit, however, ... "
Key Phrases:
General Electric, International Standard Atmosphere, Rolls-Royce Trent, Air Force, Los Angeles, compressor delivery temperature, cooling air flow rate, core jet velocity, bypass ratio increases, fan pressure ratio, inlet stagnation pressure, new large aircraft
(see more)
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Turbomachinery: Design and Theory (Mechanical Engineering (Marcell Dekker))
by Rama S.R. Gorla
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with references to "inlet stagnation pressure".
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