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 319
... units as well as pre- viously formulated and accepted derived units . Frequently used derived units with special names are listed in Table A.2 . Figure A.1 | Definition of the plane angle SI unit , radian , and the solid angle SI unit ...
... units as well as pre- viously formulated and accepted derived units . Frequently used derived units with special names are listed in Table A.2 . Figure A.1 | Definition of the plane angle SI unit , radian , and the solid angle SI unit ...
Page 320
... units exist , which are listed in Table A.3 . Table A.3 | SI prefixes1 Multiplication factor Multiplication Prefix Symbol factor Prefix Symbol 1018 exa E 10-18 1015 atto a peta P 10 ... Unit Systems and Unit Conversion Factors English Units.
... units exist , which are listed in Table A.3 . Table A.3 | SI prefixes1 Multiplication factor Multiplication Prefix Symbol factor Prefix Symbol 1018 exa E 10-18 1015 atto a peta P 10 ... Unit Systems and Unit Conversion Factors English Units.
Page 321
... units . 5 5 9 ( TOF + 459.67 ) = TOR [ A.4 ] ° R 9 = [ A.5 ] Table A.5 | Unit conversion factors Angle ( Planar ) 1 degree 60 ' = 3,600 " 1 arc minute == = 0.01745329 rad ( 1/60 ) ° = 60 ′′ = 0.01745329 rad 1 arc second = ( 1 / 3,600 ) ...
... units . 5 5 9 ( TOF + 459.67 ) = TOR [ A.4 ] ° R 9 = [ A.5 ] Table A.5 | Unit conversion factors Angle ( Planar ) 1 degree 60 ' = 3,600 " 1 arc minute == = 0.01745329 rad ( 1/60 ) ° = 60 ′′ = 0.01745329 rad 1 arc second = ( 1 / 3,600 ) ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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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