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 127
... specific heat coefficient is a known property of air . We solve Equation ( 6.16 ) for the value of the fuel - to - air ratio , which allows us to precisely determine the engine's specific fuel consumption . As explained in Chapter 4 ...
... specific heat coefficient is a known property of air . We solve Equation ( 6.16 ) for the value of the fuel - to - air ratio , which allows us to precisely determine the engine's specific fuel consumption . As explained in Chapter 4 ...
Page 144
... Specific Thrust Thrust Specific Fuel Consumption Simulations KN S kg kg KN S Equations of Motion Movie Pitch Stability & Trim Movie 10 100 Compressor Pressure Ratio 0.80 Thrust - Velocity Engine Specs Efficiencies Simulation Ven Diagram ...
... Specific Thrust Thrust Specific Fuel Consumption Simulations KN S kg kg KN S Equations of Motion Movie Pitch Stability & Trim Movie 10 100 Compressor Pressure Ratio 0.80 Thrust - Velocity Engine Specs Efficiencies Simulation Ven Diagram ...
Page 146
... specific thrust ? What is the thrust specific fuel consumption ? ( b ) What does increasing the compressor efficiency achieve ? ( c ) An increase in Mach number has what effect on thrust specific fuel consumption and specific thrust ...
... specific thrust ? What is the thrust specific fuel consumption ? ( b ) What does increasing the compressor efficiency achieve ? ( c ) An increase in Mach number has what effect on thrust specific fuel consumption and specific thrust ...
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