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 109
... joint C and joint B is FCB . The internal force in the bar between joint C and joint A is FCA Show the bar forces as tensile forces ( i.e. , pulling away from the joint ) . Tension is indicated by + and compression is indicated by ...
... joint C and joint B is FCB . The internal force in the bar between joint C and joint A is FCA Show the bar forces as tensile forces ( i.e. , pulling away from the joint ) . Tension is indicated by + and compression is indicated by ...
Page 265
... joint is the area of the cylinder cross section A times the joint length L : π V1 = AL = [ 11.3 ] where D is the cylinder diameter . Assuming that the cross section remains circular and the inner and outer edges can be approximated as ...
... joint is the area of the cylinder cross section A times the joint length L : π V1 = AL = [ 11.3 ] where D is the cylinder diameter . Assuming that the cross section remains circular and the inner and outer edges can be approximated as ...
Page 266
... joints in a spacesuit are cal- culated and tabulated in Table 11.3 . These data reveal joint operation forces which are almost at the crew member's maximum capability , or in the case of the waist joint , show that waist bending would ...
... joints in a spacesuit are cal- culated and tabulated in Table 11.3 . These data reveal joint operation forces which are almost at the crew member's maximum capability , or in the case of the waist joint , show that waist bending would ...
Table des matières
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Droits d'auteur | |
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Expressions et termes fréquents
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