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. |
À l'intérieur du livre
Résultats 1-3 sur 74
Page 71
... equation Fradial mv tan r = mviano [ 4.5 ] where Vtan is the tangential velocity and equal to v in our case . Setting Equation ( 4.4 ) and Equation ( 4.5 ) equal , we obtain mvė = L - mg cos 0 [ 4.6 ] Dividing both sides of the equation ...
... equation Fradial mv tan r = mviano [ 4.5 ] where Vtan is the tangential velocity and equal to v in our case . Setting Equation ( 4.4 ) and Equation ( 4.5 ) equal , we obtain mvė = L - mg cos 0 [ 4.6 ] Dividing both sides of the equation ...
Page 80
... equation and replace L / D by C / CD , which we assume to be equal : dm μ = dt [ 4.43 ] m CL / CD We can now integrate both sides of the equation mo dm J - 4 mo + my = μ m C / CD where E is the endurance , which yields E = CL E dt ...
... equation and replace L / D by C / CD , which we assume to be equal : dm μ = dt [ 4.43 ] m CL / CD We can now integrate both sides of the equation mo dm J - 4 mo + my = μ m C / CD where E is the endurance , which yields E = CL E dt ...
Page 132
... Equation ( 6.16 ) ] . The equation for the exit velocity was developed in Section 6.3.6 , " Nozzles , " and depends on the thermodynamic properties of total temper- ature in the nozzle and the nozzle pressure ratio ( NPR ) [ given in ...
... Equation ( 6.16 ) ] . The equation for the exit velocity was developed in Section 6.3.6 , " Nozzles , " and depends on the thermodynamic properties of total temper- ature in the nozzle and the nozzle pressure ratio ( NPR ) [ given in ...
Table des matières
A Brief History of Flight | 1 |
Introduction to Engineering | 20 |
Aerodynamics | 36 |
Droits d'auteur | |
21 autres sections non affichées
Autres éditions - Tout afficher
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