Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 pages 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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Page 78
... mass of aircraft without fuel , kg = mass of fuel , kg = □ m , fuel mass flow rate , kg / s mf The quantities mo and m , are self - explanatory ; the fuel mass flow rate is the amount of fuel ( measured by mass ) that the engines ...
... mass of aircraft without fuel , kg = mass of fuel , kg = □ m , fuel mass flow rate , kg / s mf The quantities mo and m , are self - explanatory ; the fuel mass flow rate is the amount of fuel ( measured by mass ) that the engines ...
Page 134
... mass and assuming an isothermal atmosphere , we begin by writing ue F = тио ( Μο - [ 6.29 ] We assume that at stage 2 , the compressor , the mass flow is density times veloc- ity times area A , and we substitute into Equation ( 6.29 ) ...
... mass and assuming an isothermal atmosphere , we begin by writing ue F = тио ( Μο - [ 6.29 ] We assume that at stage 2 , the compressor , the mass flow is density times veloc- ity times area A , and we substitute into Equation ( 6.29 ) ...
Page 135
... mass flow is nearly equal to the freestream mass flow , since very little 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 ...
... mass flow is nearly equal to the freestream mass flow , since very little 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 ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
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Expressions et termes fréquents
aerodynamic aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere axis balloon body Boeing burner calculate camber CD-ROM chapter coefficient coefficient of lift components compressor crew member debris Decavitator drag drawing efficiency elliptical energy Equation equilibrium example Figure flight force freestream fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift load factor low Earth orbit LTA vehicle lunar maneuver mass flow materials maximum microgravity mission motion NASA nozzle object operational orbital mechanics oxygen particles payload performance plane planetary pressure problem produced propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight specific speed stability static structural surface temperature thermal thrust truss turbine turbofan turbojet United vector velocity wing