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 44
... flow kinetic energy pv2 , and reference conditions associated with where the flow came from . In this simple form , Equation ( 3.14 ) becomes 0 1 P + = Po [ 3.15 ] where Po is a constant for the entire flow and is usually called the ...
... flow kinetic energy pv2 , and reference conditions associated with where the flow came from . In this simple form , Equation ( 3.14 ) becomes 0 1 P + = Po [ 3.15 ] where Po is a constant for the entire flow and is usually called the ...
Страница 47
... flow turn- ing caused by a given shape . It is more difficult for complex geometries , but for some simple shapes the velocity variation can be determined . Once the velocity distribution is known , the Bernoulli equation can be used ...
... flow turn- ing caused by a given shape . It is more difficult for complex geometries , but for some simple shapes the velocity variation can be determined . Once the velocity distribution is known , the Bernoulli equation can be used ...
Страница 53
... flow over an airfoil . Pressure drag can be reduced by delaying sep- aration , as in the case of the design of ... flow separates and becomes turbulent . The dimpled surface design has greater skin friction drag , but the flow separates ...
... flow over an airfoil . Pressure drag can be reduced by delaying sep- aration , as in the case of the design of ... flow separates and becomes turbulent . The dimpled surface design has greater skin friction drag , but the flow separates ...
Съдържание
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Авторско право | |
21 други раздела не са показани
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aerodynamic aerospace aircraft airfoil airplane altitude angle of attack antenna Apollo astronauts atmosphere balloon body calculated CD-ROM chapter coefficient components compressor crew member Decavitator defined density design process drag drawing ellipse energy Equation example Figure flight force fuel gravity human human spaceflight inlet International Space Station jet engine joint launch lift lines low Earth orbit LTA vehicle lunar magnetic field magnetosphere maneuver materials maximum microgravity mission module motion multiview NASA nozzle object onboard operational orbital mechanics oxygen parameters particles payload percent performance plane planetary pressure problem propeller propulsion radiation ratio rocket satellite semimajor axis simulation Skylab solar space environment Space Shuttle space station spacecraft spaceflight spacesuit design specific speed stability structural subsystem surface temperature thermal thrust turbine units Van Allen belts vector vehicle design velocity wing
Библиография
| Заглавие | Interactive Aerospace Engineering and Design Aeronautical and Aerospace Engineering Series McGraw-Hill series in aeronautical and aerospace engineering Regulatory Manual Series |
| Автор | Dava J. Newman |
| Издание | илюстрирано |
| Издател | McGraw-Hill, 2002 |
| Оригиналът е от | Мичиганският университет |
| Цифровизирана на | 14 Дек 2007 |
| ISBN | 0072348208, 9780072348200 |
| Брой страници | 356 страници |
| Експортиране на описанието | BiBTeX EndNote RefMan |