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 62
... angle at 2.5 ° and record lift . Repeat , setting the angle for 5.0 ° , 7.5 ° , and 10 ° and record the lift for each setting . Graph your results by hand . At what point will the airfoil not turn a flow ? Complete your graph with a ...
... angle at 2.5 ° and record lift . Repeat , setting the angle for 5.0 ° , 7.5 ° , and 10 ° and record the lift for each setting . Graph your results by hand . At what point will the airfoil not turn a flow ? Complete your graph with a ...
Страница 70
... angle theta to the horizon . Drag Lift Weight Thrust 0 The state variables are the velocity v , the flight path angle 0 , the horizontal position x , and the altitude h . Only one of these four requires some explanation . The flight ...
... angle theta to the horizon . Drag Lift Weight Thrust 0 The state variables are the velocity v , the flight path angle 0 , the horizontal position x , and the altitude h . Only one of these four requires some explanation . The flight ...
Страница 319
Dava J. Newman. The units for plane angle and solid angle are supplementary in SI . The radian is defined as the plane angle between two radii of a circle which cut off on the circumference an arc equal in length to the radius . The ...
Dava J. Newman. The units for plane angle and solid angle are supplementary in SI . The radian is defined as the plane angle between two radii of a circle which cut off on the circumference an arc equal in length to the radius . The ...
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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Често срещани думи и фрази
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 |