Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 страници This text contains an integrated bound-in CD-ROM, and has a strong emphasis on design. Its active visual approach and inclusion of space-orientated engineering make it an interesting examination of the aerospace engineering field. |
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Страница 78
... fuel , kg = fuel mass flow rate , kg / s The quantities mo and m , are self - explanatory ; the fuel mass flow rate is the amount of fuel ( measured by mass ) that the engines use per unit time . The gross mass of the aircraft is the ...
... fuel , kg = fuel mass flow rate , kg / s The quantities mo and m , are self - explanatory ; the fuel mass flow rate is the amount of fuel ( measured by mass ) that the engines use per unit time . The gross mass of the aircraft is the ...
Страница 127
... fuel is added in the burner domain , we account for the added mass of the fuel by using a ratio ƒ of fuel to air mass flow . The heat release Q depends on the par- ticular fuel that is being burned and is determined experimentally . The ...
... fuel is added in the burner domain , we account for the added mass of the fuel by using a ratio ƒ of fuel to air mass flow . The heat release Q depends on the par- ticular fuel that is being burned and is determined experimentally . The ...
Страница 135
... fuel is added to the stream . The thrust equation given in Equation ( 6.1 ) contains two interesting terms . Aerospace engineers often refer to the first term ( exit mass flow rate times exit velocity ) as the gross thrust since this ...
... fuel is added to the stream . The thrust equation given in Equation ( 6.1 ) contains two interesting terms . Aerospace engineers often refer to the first term ( exit mass flow rate times exit velocity ) as the gross thrust since this ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
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