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Fanno line

Detonation, Fanno Line. The Fanno -cure is used to represent the Rankine-Hugoniot mass energy equations (together with the medium equation of state) in an enthalpy-entropy plot (See Fig from Ref 1). In this [Pg.348]

Detonation (and Explosion), Flame (or Light) in. See Detonation (and Explosion), Luminosity (or Luminescence) Produced on [Pg.348]

The temperature or enthalpy of the gas may then be plotted to a base of entropy to give a Fanno line.iA This line shows the condition of the fluid as it flows along the pipe. If the velocity at entrance is subsonic (the normal condition), then the enthalpy will decrease along the pipe and the velocity will increase until sonic velocity is reached. If the flow is supersonic at the entrance, the velocity will decrease along the duct until it becomes sonic. The entropy has a maximum value corresponding to sonic velocity as shown in Figure 4.11. (Mach number Ma < 1 represents sub-sonic conditions Ma > 1 supersonic.)... [Pg.172]

Fanno lines are also useful in presenting conditions in nozzles, turbines, and other units where supersonic flow arises.(5)... [Pg.172]

P.P.S. system 3. 5 Fahrenheit units 3 False body fluids 112 Fanno lines 172 Fans 344... [Pg.876]

Since the fluid properties are defined by the entropy and enthalpy, Eqs. (9-50) represent a curve on an h—s diagram, which is called a Fanno line. [Pg.280]

Figure 9-3 Fanno line functions for k = 1.4. ([a] From Hall, 1951 and [b] from Shapiro, 1953.)... Figure 9-3 Fanno line functions for k = 1.4. ([a] From Hall, 1951 and [b] from Shapiro, 1953.)...
Fanno Line Tables for Adiabatic Flow of Air in a Constant Area Duct... [Pg.543]

Table 1-1 Fanno Line—Adiabatic, Constant Area Flow (k = 1.400) ... Table 1-1 Fanno Line—Adiabatic, Constant Area Flow (k = 1.400) ...
For adiabatic flow in a constant area duct, that is pu = constant, one has for the Fanno line... [Pg.34]

Dunkle s Syllabus (1957-1958), pp 99-102 (The Rayleigh-Mikhel son and Fanno lines) 108-10 (Flame stabilization and flameholders) 115-19 (Laminar turbulent burning) 126-27 (Coalescence of shock and combustion wave) ... [Pg.161]

Dunkle s Syllabus (1960-1961), p 9 (Addnl info on Rayleigh-Mikhel son and Fanno lines) ... [Pg.161]

Note 10 The so-called Fanno Line, briefly described by.Dunkle (Ref 93, pp 101-02) was more fully discussed by Shapiro (Ref 63a). [Pg.607]

It is briefly discussed in this write-up under Detonation, Fanno Line in... [Pg.607]

Reynolds number, p 46), etc 61-72 (Shock relationships and formulas) 73-98 (Shock wave interactions formulas) 99-102 (The Rayleigh and Fanno lines) Ibid (1958) 159-6l(Thermal theory of initiation) 168-69 (One-dimensional steady-state process) 169-72 (The Chapman-Jouguet condition) 172-76 (The von Neumann spike) 181-84 (Equations of state and covolume) 184-87 (Polytropic law) 188, 210 212 (Curved front theory of Eyring) 191-94 (The Rayleigh transformation in deton) 210-12 (Nozzle thepry of H. Jones) 285-88 (The deton head model) ... [Pg.617]

Fanno line and Rayleigh-Mikkel son line 4 D348... [Pg.624]

If flow restrictions are distributed throughout the system, other techniques, such as Fanno line analysis, must be used to estimate average gas flow rate. [Pg.328]

The effect of line friction on the pressure head available at the orifice was calculated from Fanno Line theory. [Pg.390]

See other pages where Fanno line is mentioned: [Pg.173]    [Pg.283]    [Pg.545]    [Pg.547]    [Pg.549]    [Pg.551]    [Pg.34]    [Pg.34]    [Pg.35]    [Pg.348]    [Pg.388]    [Pg.541]    [Pg.388]    [Pg.388]    [Pg.388]    [Pg.388]    [Pg.173]    [Pg.389]   
See also in sourсe #XX -- [ Pg.280 , Pg.284 ]



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