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 202
... ellipse , parabola , and hyperbola are often called conic sections , because they can all be obtained as sections cut from a right circular cone by a plane . The type of conic depends on the dihedral angle between the cutting plane and ...
... ellipse , parabola , and hyperbola are often called conic sections , because they can all be obtained as sections cut from a right circular cone by a plane . The type of conic depends on the dihedral angle between the cutting plane and ...
Page 204
... ellipse can be described as one - half the length of the longitudinal axis of the ellipse . The eccen- tricity e defines the shape of the orbit ; it is quantified as the apogee radius ( max- imum ) minus the perigee radius ( minimum ) ...
... ellipse can be described as one - half the length of the longitudinal axis of the ellipse . The eccen- tricity e defines the shape of the orbit ; it is quantified as the apogee radius ( max- imum ) minus the perigee radius ( minimum ) ...
Page 205
... ellipse ( at perigee and apogee for an earth orbit ) . A perpendicular from the semimajor axis is erected from point R , passing through the orbital position , P , of the body on the ellipse and intersecting the great circle at Q. A ...
... ellipse ( at perigee and apogee for an earth orbit ) . A perpendicular from the semimajor axis is erected from point R , passing through the orbital position , P , of the body on the ellipse and intersecting the great circle at Q. A ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
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Expressions et termes fréquents
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