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Lets talk Turbines

  1. Apr 17, 2005 #1
    Lets talk (Wren) Turbines..

    http://www.wren-turbines.com/specifi.htm
    How would you convert 81 Newtons Thrust output to power output in watts ??
     
    Last edited: Apr 17, 2005
  2. jcsd
  3. Apr 18, 2005 #2

    FredGarvin

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    Jet engines have a thrust horsepower calculation, but I don't think it could be held applicable in this case. The rule is at 375 mph, 1 Lbf of thrust is equal to 1 HP.
     
  4. Apr 19, 2005 #3
    These Wren turbines are just under three inches in diameter..
    very cool stuff..
     
  5. Apr 19, 2005 #4

    Q_Goest

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    Hey Fred, that works out, because if you say an aircraft is flying at 375 mph and that aircraft requires 1 lbf of thrust to keep it going at that speed, the power (force times distance per unit time) works out to 1 hp. But that's an arbitrary velocity. If the aircraft has more resistance, and can only fly at 100 mph with the same engine, then the equation results in a power output of 0.2667 hp. And if it's zipping along at 1000 mph, the power output becomes 2.667 hp.

    So there doesn't seem to be a correlation between hp and thrust. But there should be since the power actually equates to energy in (ie: energy burned in the engine).

    I always wondered about this one, how can you equate thrust to hp? Perhaps because it's "static thrust" one must be able to get a "thrust curve" which is analogous to a pressure curve on a centrifugal pump, along with an efficiency.

    There has to be more to it than simply thrust at 375 mph equates to a given hp.
     
  6. Apr 20, 2005 #5

    FredGarvin

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    You do bring up good points. Personally I have NEVER expressed a thrust producing engine in terms of horsepower. It is always in thrust. For some (unknown to me) reason there is a small need to express HP in this fashion. The relationship [tex] THP = \frac{F_n * MPH}{375}[/tex] is actually from a Pratt and Whitney reference I have. It is the only reference I have that even states it. What it's method of derivation is I really do not know.
     
  7. Sep 21, 2005 #6
    Oops my mistake..
    please disregard..
     
  8. Sep 23, 2005 #7

    Danger

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    As I understand it, hp:thrust ratio depends on not only speed, but also altitude. I assume that it has something to do with factoring in air resistance.
    It always bugs me that a full-throttle jet bolted to a test stand produces zero horesepower.
     
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