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 50
... motion between the object and the fluid . If there is no motion , then there is no drag . It makes no difference whether the object moves through a static fluid or the fluid moves past a static solid object . Drag acts in a direction ...
... motion between the object and the fluid . If there is no motion , then there is no drag . It makes no difference whether the object moves through a static fluid or the fluid moves past a static solid object . Drag acts in a direction ...
Страница 69
... motion which are ordinary differential equations ( ODEs ) that describe the motion ( i.e. , path ) of the aircraft . The variables in these differential equations can be divided into two groups : state variables and control variables ...
... motion which are ordinary differential equations ( ODEs ) that describe the motion ( i.e. , path ) of the aircraft . The variables in these differential equations can be divided into two groups : state variables and control variables ...
Страница 72
Dava J. Newman. EXAMPLE 4.1 Equations of motion . JPG These four equations of motion constitute our two - dimensional aircraft model , but we must discuss the limitations of the model before initiating aircraft performance analysis . In ...
Dava J. Newman. EXAMPLE 4.1 Equations of motion . JPG These four equations of motion constitute our two - dimensional aircraft model , but we must discuss the limitations of the model before initiating aircraft performance analysis . In ...
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A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
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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