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 65
... performance by deriving the operable range of speeds for aircraft as well as the range and endurance of flight vehicles . An introduction ... Performance Aircraft Performance 1 2 Introduction Performance Parameters 3 Method of Sections.
... performance by deriving the operable range of speeds for aircraft as well as the range and endurance of flight vehicles . An introduction ... Performance Aircraft Performance 1 2 Introduction Performance Parameters 3 Method of Sections.
Page 72
... performance analysis . In the process of deriving the two - dimensional model , we have made sev- eral assumptions of which we need to be fully aware . Those assumptions limit our model to only specific applications . First , the ...
... performance analysis . In the process of deriving the two - dimensional model , we have made sev- eral assumptions of which we need to be fully aware . Those assumptions limit our model to only specific applications . First , the ...
Page 247
... performance are addressed . Human presence on space missions offers many advantages to accomplish mission success . An astronaut present at the work site has the following capa- bilities : flexibility , dexterous manipulation , human ...
... performance are addressed . Human presence on space missions offers many advantages to accomplish mission success . An astronaut present at the work site has the following capa- bilities : flexibility , dexterous manipulation , human ...
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