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 65
... performance by deriving the operable range of speeds for aircraft as well as the range and endurance of flight vehicles . An introduction to the various components ... Performance Aircraft Performance 1 2 Introduction Performance Parameters.
... performance by deriving the operable range of speeds for aircraft as well as the range and endurance of flight vehicles . An introduction to the various components ... Performance Aircraft Performance 1 2 Introduction Performance Parameters.
Страница 72
... performance analysis . In the process of deriving the two - dimensional model , we have made sev- eral assumptions of which we need to be fully aware . Those assumptions limit our model to only specific applications . First , the ...
... performance analysis . In the process of deriving the two - dimensional model , we have made sev- eral assumptions of which we need to be fully aware . Those assumptions limit our model to only specific applications . First , the ...
Страница 144
... Performance Simulation Turbofan Performance Calculator Specific Thrust Thrust Specific Fuel Consumption Simulations KN S kg Equations of Motion Movie Pitch Stability & Trim Movie Thrust - Velocity Simulation 10 Compressor Pressure Ratio ...
... Performance Simulation Turbofan Performance Calculator Specific Thrust Thrust Specific Fuel Consumption Simulations KN S kg Equations of Motion Movie Pitch Stability & Trim Movie Thrust - Velocity Simulation 10 Compressor Pressure Ratio ...
Съдържание
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