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 73
... Simulation A thrust - velocity ( T - v ) simulation tool is provided on the CD - ROM . Use the simula- tor to characterize a Boeing 727 in steady , level flight . ( See Figure 4.4 . ) Given : Thrust available , TA = 186,825 N ; weight W ...
... Simulation A thrust - velocity ( T - v ) simulation tool is provided on the CD - ROM . Use the simula- tor to characterize a Boeing 727 in steady , level flight . ( See Figure 4.4 . ) Given : Thrust available , TA = 186,825 N ; weight W ...
Page 90
Dava J. Newman. EXAMPLE 4.6 The V - n simulation V - n diagram simulation . Using the velocity - load ( V - n ) simulation tool on the CD - ROM , find the flight envelope for a Boeing 727 aircraft with the following characteristics ...
Dava J. Newman. EXAMPLE 4.6 The V - n simulation V - n diagram simulation . Using the velocity - load ( V - n ) simulation tool on the CD - ROM , find the flight envelope for a Boeing 727 aircraft with the following characteristics ...
Page 144
... Simulation Turbofan Performance Calculator 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 ...
... Simulation Turbofan Performance Calculator 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 ...
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