Corrected fuel flow
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Corrected fuel flow is the fuel flow that is required by an engine if the freestream total head conditions are equivalent to ambient conditions at Sea Level on a Standard Day (i.e. 14.696lb/in², 288.15K ).
Corrected Fuel Flow can be calculated as follows, assuming Imperial units:
So-called Non-Dimensional Fuel Flow
) is proportional to Corrected Fuel Flow:
Corrected Fuel Flow (or Non-Dimensional Fuel Flow) is one of several non-dimensional groups associated with gas turbine performance calculations.
The equivalent equations for Preferred SI Units are:
Nomenclature:
- P Stagnation (or Total) Pressure
- T Stagnation (or Total) Temperature
[edit] References
| This article needs additional citations for verification. Please help improve this article by adding reliable references. Unsourced material may be challenged and removed. (August 2007) |
- Padilla, Carlos E. (1996). Optimizing Jet Transport Efficiency: Performance, Operations, and Economics. McGraw-Hill Professional, page 31. ISBN 007048208X.
![wfe/({\delta}.\sqrt{\theta}) = wfe/[(P/14.696).(\sqrt{T}/\sqrt{288.15})]](../../../../math/1/f/a/1fa7ad7744c046422dee2ac38df48bfd.png)
![wfe/({P}.\sqrt{T})= [wfe/({\delta}.\sqrt{\theta})] * \sqrt{288.15}/{14.696})](../../../../math/8/2/0/8207c96d1607500234624ec52ee4ed6e.png)
![wfe/({\delta}.\sqrt{\theta}) = wfe/[(P/101.325).(\sqrt{T}/\sqrt{288.15})]](../../../../math/1/a/7/1a7317aecd45a610562f5e58bf765977.png)
![wfe/({P}.\sqrt{T})= [wfe/({\delta}.\sqrt{\theta})] * (\sqrt{288.15}/{101.325})](../../../../math/5/f/2/5f20885546125f4de8df5e84d2e03795.png)

