Interactive Aerospace Engineering and DesignThis 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 73
... Calculate the lift coefficient C , for a given velocity v , by recalling the def- inition of dynamic pressure q = 1 / 2pv2 : CL = 2W Pov2s 3. Calculate the drag coefficient from the drag polar for the aircraft . Ci Co = Coo + TEAR ...
... Calculate the lift coefficient C , for a given velocity v , by recalling the def- inition of dynamic pressure q = 1 / 2pv2 : CL = 2W Pov2s 3. Calculate the drag coefficient from the drag polar for the aircraft . Ci Co = Coo + TEAR ...
Page 77
... calculate ( L / D ) max by writing [ 4.28 ] Type of aircraft ( L / D ) max Modern sailplanes 25-40 [ 4.29 ] Civil jet 12-20 D ( ) = max CL 2C / ( TEAR ) TEAR = 2CL . ( L / D ) max Typical values of the maximum lift - to - drag ratio for ...
... calculate ( L / D ) max by writing [ 4.28 ] Type of aircraft ( L / D ) max Modern sailplanes 25-40 [ 4.29 ] Civil jet 12-20 D ( ) = max CL 2C / ( TEAR ) TEAR = 2CL . ( L / D ) max Typical values of the maximum lift - to - drag ratio for ...
Page 92
... Calculate the minimum landing speed that a short- to medium - range jetliner , modeled after the Boeing 737-300 , can have when landing at the Denver , Colorado , International Airport when its landing weight is 40,000 kg . The wing ...
... Calculate the minimum landing speed that a short- to medium - range jetliner , modeled after the Boeing 737-300 , can have when landing at the Denver , Colorado , International Airport when its landing weight is 40,000 kg . The wing ...
Contents
A Brief History of Flight | 1 |
Chapter | 4 |
Introduction to Engineering | 20 |
Copyright | |
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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