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  • Jet Propulsion/General cascade analysis
    The [[Jet propulsion/Total enthalpy|total enthalpy]] h_t of the fluid flowing at velocity u is [[Jet propulsion/Euler turbine equation|Euler turbine equation]] ...
    315 bytes (50 words) - 17:59, 7 September 2007
  • Jet Propulsion/Mechanics
    ==[[Jet Propulsion/Engine_ratings|Engine ratings]]== ==[[Jet Propulsion/Specific impulse|Specific impulse]]== ...
    3 KB (533 words) - 18:00, 7 September 2007
  • Jet Propulsion/Total enthalpy
    [[Category:Jet Propulsion]] ...
    118 bytes (24 words) - 17:59, 7 September 2007
  • Jet Propulsion/Thermodynamic Cycles
    ...air and combustion products which are then accelerated to provide reaction propulsion. ...ive applications the definition of efficiency involves the velocity of the jet through the air since a stationary engine anchored to the ground produces n ...
    5 KB (815 words) - 18:00, 7 September 2007
  • Jet Propulsion/Thermodynamic Cycles/Ramjet cycle
    A ramjet uses the open [[Jet Propulsion/Thermodynamic Cycles/Brayton cycle|Brayton cycle]]. In the above diagram a [[Category:Jet Propulsion]] ...
    1 KB (161 words) - 18:00, 7 September 2007
  • Jet Propulsion/Cascade analysis
    [[Category:Jet Propulsion]] ...
    273 bytes (39 words) - 18:00, 7 September 2007
  • Jet Propulsion/Propulsive efficiency
    ...frame of reference the input mass flow has zero kinetic energy. Thus for a jet engine with a constant relative exit velocity (a close approximation of a [[Category:Jet Propulsion]] ...
    1 KB (226 words) - 18:00, 7 September 2007
  • Jet Propulsion/Euler turbine equation
    [[Category:Jet Propulsion]] ...
    437 bytes (72 words) - 18:00, 7 September 2007
  • Jet Propulsion/Stage temperature ratio
    [[Category:Jet Propulsion]] ...
    453 bytes (75 words) - 17:59, 7 September 2007
  • Jet Propulsion/Gas turbine energy exchange
    [[Category:Jet Propulsion]] ...
    558 bytes (84 words) - 18:00, 7 September 2007
  • Jet Propulsion/Streamline
    [[Category:Jet Propulsion]] ...
    491 bytes (77 words) - 18:00, 7 September 2007
  • Jet Propulsion/Thermal efficiency
    [[Category:Jet Propulsion]] ...
    739 bytes (112 words) - 18:00, 7 September 2007
  • Jet Propulsion/1D Analysis
    [[Category:Jet Propulsion]] ...
    1 KB (253 words) - 09:02, 1 October 2007
  • Jet Propulsion/Performance
    [[Category:Jet Propulsion]] ...
    1 KB (203 words) - 18:00, 7 September 2007
  • Rocket Propulsion:Fundamental Principles of Rocket Propulsion
    Rocket propulsion is based on Newton's three laws of motion: ...s of thrust, but are inefficient in their use of propellant. Electric ion propulsion conversely uses propellant very efficiently, but is only able to produce sm ...
    5 KB (934 words) - 04:37, 28 October 2007
  • Rocket Propulsion:Temporary
    < <b>[[Rocket Propulsion|Cover]]</b> ...en from the atmosphere is used as the oxidant for the fuel. Because rocket propulsion can generate far greater thrust and can operate in oxygen-free environments ...
    10 KB (1,698 words) - 20:45, 23 September 2007
  • Jet Propulsion/Aerodynamics
    [[Category:Jet Propulsion]] ...
    18 KB (2,940 words) - 15:56, 16 November 2007
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