Interactive Aerospace Engineering and DesignMcGraw-Hill, 2002 - 356 pagini 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. |
Din interiorul cărții
Rezultatele 1 - 3 din 11
Pagina 47
... look at lift and drag as a function of the angle of attack of the wing to get an overall appreciation of aerodynamic performance . Lift of an airplane increases as a increases until a point called the stall angle ( see Figure 3.5 ) ...
... look at lift and drag as a function of the angle of attack of the wing to get an overall appreciation of aerodynamic performance . Lift of an airplane increases as a increases until a point called the stall angle ( see Figure 3.5 ) ...
Pagina 49
... Look at the dimensionless parameter C2 [ Equation ( 3.10 ) ] and make sure to include all units . For the full - size wing , CL = For the model wing , CL = 250 kg . m / s2 ( 1.0 kg / m3 ) ( 10 m / s ) 2 ( 5 m2 ) 80 kg ⚫ m / s2 = 1.0 ...
... Look at the dimensionless parameter C2 [ Equation ( 3.10 ) ] and make sure to include all units . For the full - size wing , CL = For the model wing , CL = 250 kg . m / s2 ( 1.0 kg / m3 ) ( 10 m / s ) 2 ( 5 m2 ) 80 kg ⚫ m / s2 = 1.0 ...
Pagina 117
... look at the way aircraft engines work . All aircraft propulsion systems are based on the principle of reaction of airflow through an engine of some sort . It may also be thought of as the acceleration of air flowing through the aircraft ...
... look at the way aircraft engines work . All aircraft propulsion systems are based on the principle of reaction of airflow through an engine of some sort . It may also be thought of as the acceleration of air flowing through the aircraft ...
Cuprins
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Drept de autor | |
15 alte secțiuni nu sunt arătate
Alte ediții - Afișează-le pe toate
Termeni și expresii frecvente
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
Referințe la această carte
Intelligent Components and Instruments for Control Applications 2003 (SICICA ... L. Almeida,Luis B. Almeida,S. Boverie Previzualizare limitată - 2003 |